30°21′45.96″N 89°36′00.72″W / 30.3627667°N 89.6002000°W / 30.3627667; -89.6002000
170-676: The John C. Stennis Space Center ( SSC ) is a NASA rocket testing facility in Hancock County, Mississippi , United States , on the banks of the Pearl River at the Mississippi – Louisiana border. As of 2012, it is NASA's largest rocket engine test facility . There are over 50 local, state, national, international, private, and public companies and agencies using SSC for their rocket testing facilities. The initial requirements for NASA's proposed rocket testing facility required
340-570: A "round of main injector testing in late 2014," and a "full-power test of the oxygen preburner component" for Raptor by June 2015. The E3 test stand consists of two test cells for component and pilot scale combustion device testing: A series of tests conducted in the late 1990s eventually led to the commercialization of hybrid rocket motors. Test firing an American Rocket Company (AMROC) hybrid rocket motor at NASA's Stennis Space Center in 1994. The E4 test stand consists of four 32 foot tall concrete-walled cells and an associated concrete foundation;
510-428: A 1,344 square foot hardened and conditioned Signal Conditioning Building; a 12,825 square foot high bay with 10 ton bridge crane, shop area with 1 ton bridge crane, and a 7,000 square foot blast hardened Test Control Center; and two 1,400 square foot raised-floor control rooms. The site also includes underground deluge water piping; underground power, data, and control duct banks; and potable water. The E4 hard stand system
680-628: A decade of reliance on the Russians. In 2019, NASA announced the Artemis program , intending to return to the Moon and establish a permanent human presence. This was paired with the Artemis Accords with partner nations to establish rules of behavior and norms of space commercialization on the Moon. In 2023, NASA established the Moon to Mars Program office. The office is designed to oversee
850-401: A dry mass of about 303,000 pounds (137,000 kilograms); when fully fueled at launch, it had a total mass of 4,881,000 pounds (2,214,000 kilograms). The S-IC was powered by five Rocketdyne F-1 engines arrayed in a quincunx . The center engine was held in a fixed position, while the four outer engines could be hydraulically turned with gimbals to steer the rocket. In flight, the center engine
1020-469: A human in space, develop tracking and control systems, and identify other issues associated with human spaceflight. While much of NASA's attention turned to space, it did not put aside its aeronautics mission. Early aeronautics research attempted to build upon the X-1's supersonic flight to build an aircraft capable of hypersonic flight . The North American X-15 was a joint NASA–U.S. Air Force program, with
1190-416: A hydrogen link leak caused automatic cutoff. At time of the explosion, technicians were trying to determine cause for the hydrogen leak. No hydrogen was in the tank when the explosion occurred. Under the direction of MSFC, a Board of Inquiry headed by Dr. Kurt H. Debus, Director of Kennedy Space Center, convened on the night of May 28. Immediate investigation revealed that the second shift crew, not knowing that
1360-463: A low Earth orbit (LEO) payload capacity originally estimated at 261,000 pounds (118,000 kg), but was designed to send at least 90,000 pounds (41,000 kg) to the Moon. Later upgrades increased that capacity; on the final three Apollo lunar missions, it sent up to 95,901 lb (43,500 kg) to the Moon. At a height of 363 feet (111 m), the Saturn V stood 58 feet (18 m) taller than
1530-462: A lunar orbit rendezvous provided the simplest landing on the Moon with the most cost–efficient launch vehicle, and the best chance to accomplish the lunar landing within the decade. Other NASA officials became convinced, and LOR was then officially selected as the mission configuration for the Apollo program and announced by NASA administrator James E. Webb on November 7, 1962. Arthur Rudolph became
1700-549: A mainstage duration of 29 seconds. On March 31, failure of a prevalve to close caused program officials to scrub the first attempt to static fire the S-II-2 stage. Battleship testing of the S-II battleship test stage equipped with five uprated J-2 engines ended in late March 1967 with a full-duration test of approximately 360 seconds mainstage operation. These two test stands tested and flight-certified S-II stages and J-2 engines until
1870-649: A one-room school house, still exist within the facility. The 13,500 acres (55 km) site was selected on October 25, 1961, on the Mississippi Test Facility or Pearl River Site . On December 18, 1961, NASA officially designated the facility as NASA Mississippi Test Operations . The test area (officially known as the Fee Area ) is surrounded by a 125,000 acre (506 km) acoustical buffer zone . The facility's large concrete and metal rocket propulsion test stands were originally used to test-fire
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#17327826613272040-776: A pair of AJ26 engines. The first test of the RS-25 engine for use on the Space Launch System (SLS) rocket was conducted January 9, 2015. Stennis completed testing of all 16 heritage RS-25 engines that will help launch the first four SLS missions as part of NASA's Artemis program on April 4, 2019. The A-1 Test Stand was designated the Fred Haise Test Stand in March 2020, in honor of the Apollo 13 astronaut and Biloxi, Mississippi , native. The first test of
2210-583: A permanently manned space station and to do it within a decade. In 1985, NASA proposed the Space Station Freedom , which both the agency and President Reagan intended to be an international program. While this would add legitimacy to the program, there were concerns within NASA that the international component would dilute its authority within the project, having never been willing to work with domestic or international partners as true equals. There
2380-650: A possible source of antimatter at the center of the Milky Way and observing that the majority of gamma-ray bursts occur outside of the Milky Way galaxy. The Chandra X-ray Observatory was launched from the Columbia on STS-93 in 1999, observing black holes, quasars , supernova , and dark matter . It provided critical observations on the Sagittarius A* black hole at the center of the Milky Way galaxy and
2550-513: A proposed replacement for the first stage was the AJ-260x . This solid rocket motor would have simplified the design by removing the five-engine configuration and, in turn, reduced launch costs. The S-II was built by North American Aviation at Seal Beach, California . Using liquid hydrogen and liquid oxygen, it had five Rocketdyne J-2 engines in a similar arrangement to the S-IC, and also used
2720-426: A rocket varies with air density and the square of relative velocity . Although velocity continues to increase, air density decreases so quickly with altitude that dynamic pressure falls below max q. The propellant in just the S-IC made up about three-quarters of Saturn V's entire launch mass, and it was consumed at 13,000 kilograms per second (1,700,000 lb/min). Newton's second law of motion states that force
2890-587: A second time for translunar injection (TLI). The Saturn V's instrument unit was built by IBM and was placed on top of the rocket's third stage. It was constructed at the Space Systems Center in Huntsville, Alabama . This computer controlled the operations of the rocket from just before liftoff until the S-IVB was discarded. It included guidance and telemetry systems for the rocket. By measuring
3060-507: A second. Once the rocket had lifted off, it could not safely settle back down onto the pad if the engines failed. The astronauts considered this one of the tensest moments in riding the Saturn V, for if the rocket did fail to lift off after release they had a low chance of survival given the large amounts of propellant. To improve safety, the Saturn Emergency Detection System (EDS) inhibited engine shutdown for
3230-562: A single rocket launching two spacecraft: a mother ship , and a smaller, two-man landing module which would rendezvous back with the main spacecraft in lunar orbit. The lander would be discarded and the mother ship would return home. At first, NASA dismissed LOR as a riskier option, as a space rendezvous had yet to be performed in Earth orbit, much less in lunar orbit. Several NASA officials, including Langley Research Center engineer John Houbolt and NASA Administrator George Low , argued that
3400-434: A space station since the agency was created. In 1973, following the end of the Apollo lunar missions, NASA launched its first space station, Skylab , on the final launch of the Saturn V. Skylab reused a significant amount of Apollo and Saturn hardware, with a repurposed Saturn V third stage serving as the primary module for the space station. Damage to Skylab during its launch required spacewalks to be performed by
3570-539: A static test stand and for use in static firings. Workmen loaded the huge booster aboard the barge Poseidon for the 1,000-mile river journey. Six days later the S-IC-T reached SSC. All future firings would be accomplished at the B-2 stand. An all-systems test version of Apollo/Saturn V first stage, S-IC-T, went into the B-2 test stand at the Mississippi Test Facility on December 17, 1966. Stage electrical and mechanical hook-up to
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#17327826613273740-403: A time with a delay to reduce peak acceleration further. After S-IC separation, the S-II second stage burned for 6 minutes and propelled the craft to 109 miles (175 km) and 15,647 mph (25,181 km/h), close to orbital velocity . For the first two uncrewed launches, eight solid-fuel ullage motors ignited for four seconds to accelerate the S-II stage, followed by the ignition of
3910-427: A total of just 20 minutes. Although Apollo 6 experienced three engine failures, and Apollo 13 experienced one engine shutdown, the onboard computers were able to compensate by burning the remaining engines longer to achieve parking orbit. In the event of an abort requiring the destruction of the rocket, the range safety officer would remotely shut down the engines and after several seconds send another command for
4080-532: Is a rocket testing complex which was built in 1965 as a component of the John C. Stennis Space Center. The Rocket Propulsion Test Complex played an important role in the development of the Saturn V rocket. The A-1, A-2 and B-1/B-2 test stands were declared a National Historic Landmark in 1985. The NASA Engineering & Science Directorate (ESD) at SSC operates and maintains SSC's rocket test stands. The smaller two of
4250-404: Is equal to mass multiplied by acceleration, or equivalently that acceleration is equal to force divided by mass, so as the mass decreased (and the force increased somewhat), acceleration rose. Including gravity, launch acceleration was only 1 + 1 ⁄ 4 g , i.e., the astronauts felt 1 + 1 ⁄ 4 g while the rocket accelerated vertically at 1 ⁄ 4 g . As
4420-864: The AR-1 rocket engine could be tested there, with a goal of first flight of the new AR-1 engine after 2019. The stand is composed of three individual test "cells": The E2 test facility at Stennis has multiple test cells that support three separate test stands (Cell 1 and Cell 2), for testing horizontally-mounted engines and for vertically mounted vehicle stages and/or engines. Cell 1 can support engines with up to 100,000 pounds-force (440 kN) of thrust while Cell 2 can support vehicle stages with up to 324,000 pounds-force (1,440 kN) of thrust. The facility can provide liquid oxygen, liquid nitrogen, liquid hydrogen, liquid methane , rocket-grade kerosene (RP1), H 2 O , gaseous hydrogen, "hot" gaseous hydrogen, gaseous oxygen and gaseous nitrogen. E2 Cell 1, originally known as
4590-677: The Big Bang . The James Webb Space Telescope , named after the NASA administrator who lead the Apollo program, is an infrared observatory launched in 2021. The James Webb Space Telescope is a direct successor to the Hubble Space Telescope, intended to observe the formation of the first galaxies. Other space telescopes include the Kepler space telescope , launched in 2009 to identify planets orbiting extrasolar stars that may be Terran and possibly harbor life. The first exoplanet that
4760-797: The Environmental Science Services Administration on a series of weather satellites and the agency launched its experimental Applications Technology Satellites into geosynchronous orbit. NASA's first dedicated Earth observation satellite, Landsat , was launched in 1972. This led to NASA and the National Oceanic and Atmospheric Administration jointly developing the Geostationary Operational Environmental Satellite and discovering Ozone depletion . NASA had been pursuing spaceplane development since
4930-691: The Europa and observed that the moon may hold ice or liquid water. A joint NASA- European Space Agency - Italian Space Agency mission, Cassini–Huygens , was sent to Saturn 's moon Titan , which, along with Mars and Europa, are the only celestial bodies in the Solar System suspected of being capable of harboring life. Cassini discovered three new moons of Saturn and the Huygens probe entered Titan's atmosphere. The mission discovered evidence of liquid hydrocarbon lakes on Titan and subsurface water oceans on
5100-807: The International Space Station (ISS) along with the Commercial Crew Program , and oversees the development of the Orion spacecraft and the Space Launch System for the lunar Artemis program . NASA's science division is focused on better understanding Earth through the Earth Observing System ; advancing heliophysics through the efforts of the Science Mission Directorate 's Heliophysics Research Program; exploring bodies throughout
5270-784: The Johnson Space Center as the lead center for the design, development, and manufacturing of the Space Shuttle orbiter , while the Marshall Space Flight Center would lead the development of the launch system. NASA's series of lifting body aircraft, culminating in the joint NASA-U.S. Air Force Martin Marietta X-24 , directly informed the development of the Space Shuttle and future hypersonic flight aircraft. Official development of
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5440-588: The Launch Escape System rocket (150,000 pounds-force (667 kN) sea level thrust) mounted atop the Apollo command module. The Apollo LES fired for a much shorter time than the Mercury-Redstone (3.2 seconds vs. 143.5 seconds). The Saturn V was principally designed by the Marshall Space Flight Center in Huntsville, Alabama , although numerous major systems, including propulsion systems, were designed by subcontractors. The rocket used
5610-664: The Mars Global Surveyor orbiter and Mars Pathfinder , deploying the first Mars rover, Sojourner . During the early 2000s, the 2001 Mars Odyssey orbiter reached the planet and in 2004 the Sprit and Opportunity rovers landed on the Red Planet. This was followed in 2005 by the Mars Reconnaissance Orbiter and 2007 Phoenix Mars lander. The 2012 landing of Curiosity discovered that
5780-918: The Mississippi River to the Gulf of Mexico . After rounding Florida , the stages were transported up the Intra-Coastal Waterway to the Vehicle Assembly Building (originally called the Vertical Assembly Building). This was essentially the same route which would be used later to ship Space Shuttle external tanks . The S-II was constructed in California and traveled to Florida via the Panama Canal . The third stage and Instrument Unit
5950-555: The National Advisory Committee for Aeronautics (NACA) to give the U.S. space development effort a distinct civilian orientation, emphasizing peaceful applications in space science . It has since led most of America's space exploration programs, including Project Mercury , Project Gemini , the 1968–1972 Apollo Moon landing missions, the Skylab space station, and the Space Shuttle . Currently, NASA supports
6120-684: The National Advisory Committee for Aeronautics (NACA). Despite being the birthplace of aviation, by 1914 the United States recognized that it was far behind Europe in aviation capability. Determined to regain American leadership in aviation, the United States Congress created the Aviation Section of the U.S. Army Signal Corps in 1914 and established NACA in 1915 to foster aeronautical research and development. Over
6290-614: The Orbiting Geophysical Observatory in the 1960s and 1970s to look down at Earth and observe its interactions with the Sun. The Uhuru satellite was the first dedicated x-ray telescope, mapping 85% of the sky and discovering a large number of black holes . Launched in the 1990s and early 2000s, the Great Observatories program are among NASA's most powerful telescopes. The Hubble Space Telescope
6460-658: The STS-1 mission, designed to serve as a flight test for the new spaceplane. NASA intended for the Space Shuttle to replace expendable launch systems like the Air Force's Atlas , Delta , and Titan and the European Space Agency 's Ariane . The Space Shuttle's Spacelab payload, developed by the European Space Agency, increased the scientific capabilities of shuttle missions over anything NASA
6630-635: The STS-60 mission in 1994 and the Discovery rendezvoused, but did not dock with, the Russian Mir in the STS-63 mission. This was followed by Atlantis' STS-71 mission where it accomplished the initial intended mission for the Space Shuttle, docking with a space station and transferring supplies and personnel. The Shuttle- Mir program would continue until 1998, when a series of orbital accidents on
6800-541: The Solar System with advanced robotic spacecraft such as New Horizons and planetary rovers such as Perseverance ; and researching astrophysics topics, such as the Big Bang , through the James Webb Space Telescope , the four Great Observatories , and associated programs. The Launch Services Program oversees launch operations for its uncrewed launches . NASA traces its roots to
6970-535: The Space Race when the Soviet Union gave up its lunar ambitions. As the first human to step on the surface of the Moon, Neil Armstrong uttered the now famous words: That's one small step for man, one giant leap for mankind. NASA would conduct six total lunar landings as part of the Apollo program, with Apollo 17 concluding the program in 1972. Wernher von Braun had advocated for NASA to develop
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7140-620: The Space Shuttle began in 1972, with Rockwell International contracted to design the orbiter and engines, Martin Marietta for the external fuel tank , and Morton Thiokol for the solid rocket boosters . NASA acquired six orbiters: the Enterprise , Columbia , Challenger , Discovery , Atlantis , and Endeavour The Space Shuttle program also allowed NASA to make major changes to its Astronaut Corps . While almost all previous astronauts were Air Force or Naval test pilots,
7310-732: The Statue of Liberty from the ground to the torch, and 48 feet (15 m) taller than the Elizabeth Tower , which houses Big Ben at the Palace of Westminster . In contrast, the Mercury-Redstone Launch Vehicle used on Freedom 7 , the first crewed American spaceflight, was approximately 11 feet (3.4 m) longer than the S-IVB stage and delivered less sea level thrust (78,000 pounds-force (350 kN)) than
7480-405: The inner planets . Despite these successes, Congress was unwilling to fund further interplanetary missions and NASA Administrator James Webb suspended all future interplanetary probes to focus resources on the Apollo program. Following the conclusion of the Apollo program, NASA resumed launching interplanetary probes and expanded its space science program. The first planet tagged for exploration
7650-557: The instrument unit . All three stages used liquid oxygen (LOX) as the oxidizer . The first stage used RP-1 for fuel, while the second and third stages used liquid hydrogen (LH2). LH2 has a higher specific energy (energy per unit mass) than RP-1, which makes it more suitable for higher-energy orbits, such as the trans-lunar injection required for Apollo missions. Conversely, RP-1 offers higher energy density (energy per unit volume) and higher thrust than LH2, which makes it more suitable for reducing aerodynamic drag and gravity losses in
7820-420: The 1950s as a response to Soviet lunar exploration, however most missions ended in failure. The Lunar Orbiter program had greater success, mapping the surface in preparation for Apollo landings and measured Selenography , conducted meteoroid detection, and measured radiation levels. The Surveyor program conducted uncrewed lunar landings and takeoffs, as well as taking surface and regolith observations. Despite
7990-420: The 1960s, blending the administration's dual aeronautics and space missions. NASA viewed a spaceplane as part of a larger program, providing routine and economical logistical support to a space station in Earth orbit that would be used as a hub for lunar and Mars missions. A reusable launch vehicle would then have ended the need for expensive and expendable boosters like the Saturn V . In 1969, NASA designated
8160-679: The 44 commercial companies that contracted with NASA to deploy their satellites to return to expendable launch vehicles. When the Space Shuttle returned to flight with the STS-26 mission, it had undergone significant modifications to improve its reliability and safety. Following the collapse of the Soviet Union, the Russian Federation and United States initiated the Shuttle- Mir program . The first Russian cosmonaut flew on
8330-519: The A-3 stand to develop and test their Archimedes reusable rocket engine. In the 1990s, a new test complex named "E" was constructed to test a variety of new small engine and single/multiple components and concepts. The E test stand complex consists of four distinct test stands In 2012, Blue Origin tested the thrust chamber assembly at the E-1 test cell for its new 100,000 pounds-force (440 kN) thrust BE-3 liquid oxygen/liquid hydrogen rocket engine. As part of Blue's Reusable Booster System (RBS),
8500-403: The Army's Project Adam, served as the foundation for Project Mercury . NASA established the Space Task Group to manage the program, which would conduct crewed sub-orbital flights with the Army's Redstone rockets and orbital flights with the Air Force's Atlas launch vehicles. While NASA intended for its first astronauts to be civilians, President Eisenhower directed that they be selected from
8670-458: The Army's rocket design division. Between 1945 and 1958, his work was restricted to conveying the ideas and methods behind the V-2 to American engineers, though he wrote books and articles in popular magazines. This approach changed in 1957, when the Soviets launched Sputnik 1 atop an R-7 ICBM, which could carry a thermonuclear warhead to the U.S. The Army and government began putting more effort towards sending Americans into space before
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#17327826613278840-399: The C-4, which would use four F-1 engines in its first stage, an enlarged C-3 second stage, and the S-IVB , a stage with a single J-2 engine, as its third stage. The C-4 would only need to carry out two launches to carry out an EOR lunar mission. On January 10, 1962, NASA announced plans to build the C-5. The three-stage rocket would consist of the S-IC first stage, with five F-1 engines;
9010-408: The C-5. Rather than undergoing testing for each major component, the C-5 would be tested in an "all-up" fashion, meaning that the first test flight of the rocket would include complete versions of all three stages. By testing all components at once, far fewer test flights would be required before a crewed launch. The C-5 was confirmed as NASA's choice for the Apollo program in early 1962, and was named
9180-450: The E2 test stand had been a 2012 NASA test of chemical steam generators . Beginning in 2014, SpaceX conducted component tests of their liquid methane/liquid oxygen Raptor rocket engine on the E2 test stand. This testing was limited to components of the Raptor engine, since the test stand is not large enough to test the full Raptor engine, which is rated to generate more than 661,000 lbf (2,940 kN) vacuum thrust. SpaceX completed
9350-411: The High Heat Flux Facility (HHFF), was constructed in 1993 to support materials development for the National Aerospace Plane (NASP). The E2 test stand was modified after 2013 to support liquid methane engine testing, with funds being provided by SpaceX , the Mississippi Development Authority ( US$ 500,000 using funding from state bond issues), and NASA (up to US$ 600,000 ). As of October 2013,
9520-425: The Jupiter vehicles. Between 1960 and 1962, the Marshall Space Flight Center (MSFC) designed a series of Saturn rockets that could be deployed for Earth orbit and lunar missions. NASA planned to use the Saturn C-3 as part of the Earth orbit rendezvous (EOR) method for a lunar mission, with at least two or three launches needed for a single landing on the Moon. However, the MSFC planned an even bigger rocket,
9690-439: The Keplar space telescope confirmed was Kepler-22b , orbiting within the habitable zone of its star. NASA also launched a number of different satellites to study Earth, such as Television Infrared Observation Satellite (TIROS) in 1960, which was the first weather satellite. NASA and the United States Weather Bureau cooperated on future TIROS and the second generation Nimbus program of weather satellites. It also worked with
9860-448: The Martian interior. The 2021 Perseverance rover carried the first extraplanetary aircraft, a helicopter named Ingenuity . NASA also launched missions to Mercury in 2004, with the MESSENGER probe demonstrating as the first use of a solar sail . NASA also launched probes to the outer Solar System starting in the 1960s. Pioneer 10 was the first probe to the outer planets, flying by Jupiter , while Pioneer 11 provided
10030-402: The Moon and going to Mars. Embracing this approach, NASA's Commercial Crew Program started by contracting cargo delivery to the International Space Station and flew its first operational contracted mission on SpaceX Crew-1 . This marked the first time since the retirement of the Space Shuttle that NASA was able to launch its own astronauts on an American spacecraft from the United States, ending
10200-399: The Moon from Apollo 8 (December 1968) to Apollo 17 (December 1972). In September 1945, the U.S. government brought the German rocket technologist Wernher von Braun and over 1,500 German rocket engineers and technicians to the United States in Operation Paperclip , a program authorized by President Truman . Von Braun, who had helped create the German V-2 rocket, was assigned to
10370-542: The Moon. The largest production model of the Saturn family of rockets , the Saturn V was designed under the direction of Wernher von Braun at the Marshall Space Flight Center in Huntsville, Alabama ; the lead contractors for construction of the rocket were Boeing , North American Aviation , Douglas Aircraft Company , and IBM . Fifteen flight-capable vehicles were built, not counting three used for ground testing. A total of thirteen missions were launched from Kennedy Space Center , nine of which carried 24 astronauts to
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#173278266132710540-434: The Naval Research Laboratory's Project Vanguard, the Army's Jet Propulsion Laboratory (JPL), and the Army Ballistic Missile Agency under Wernher von Braun . This left NASA firmly as the United States' civil space lead and the Air Force as the military space lead. Plans for human spaceflight began in the U.S. Armed Forces prior to NASA's creation. The Air Force's Man in Space Soonest project formed in 1956, coupled with
10710-503: The Pilotless Aircraft Research Division. The Soviet Union's launch of Sputnik 1 ushered in the Space Age and kicked off the Space Race . Despite NACA's early rocketry program, the responsibility for launching the first American satellite fell to the Naval Research Laboratory 's Project Vanguard , whose operational issues ensured the Army Ballistic Missile Agency would launch Explorer 1 , America's first satellite, on February 1, 1958. The Eisenhower Administration decided to split
10880-409: The Russians be included. In 1993, the Clinton Administration announced that the Space Station Freedom would become the International Space Station in an agreement with the Russian Federation. This allowed the Russians to maintain their space program through an infusion of American currency to maintain their status as one of the two premier space programs. While the United States built and launched
11050-507: The Russians to fly to the International Space Station for four days, despite the opposition of NASA to the idea. Advocates of this new commercial approach for NASA included former astronaut Buzz Aldrin , who remarked that it would return NASA to its roots as a research and development agency, with commercial entities actually operating the space systems. Having corporations take over orbital operations would also allow NASA to focus all its efforts on deep space exploration and returning humans to
11220-469: The S-IC from the rest of the vehicle at an altitude of about 42 miles (67 km). The first stage continued on a ballistic trajectory to an altitude of about 68 miles (109 km) and then fell in the Atlantic Ocean about 350 miles (560 km) downrange. The engine shutdown procedure was changed for the launch of Skylab to avoid damage to the Apollo Telescope Mount . Rather than shutting down all four outboard engines at once, they were shut down two at
11390-405: The S-IC, the S-II was transported from its manufacturing plant to Cape Kennedy by sea. The S-IVB stage was built by the Douglas Aircraft Company at Huntington Beach, California . It had one Rocketdyne J-2 engine and used the same fuel as the S-II. The S-IVB used a common bulkhead to separate the two tanks. It was 58.6 feet (17.86 m) tall with a diameter of 21.7 feet (6.604 m) and
11560-406: The S-II second stage, with five J-2 engines; and the S-IVB third stage, with a single J-2 engine. The C-5 would undergo component testing even before the first model was constructed. The S-IVB third stage would be used as the second stage for the C-1B, which would serve both to demonstrate proof of concept and feasibility for the C-5, but would also provide flight data critical to the development of
11730-400: The S-II-1 stage ended at MTF. On January 27, 1967, the S-II-2 stage left Seal Beach, California, to pass through the Panama Canal and on to MTF. After its journey lasting 16 days, the S-II would arrive at MTF for two static tests. The S-II-2 stage arrived on dock at MTF on February 11, 1967. The S-II-2 stage, part of the second Saturn V vehicle (AS-502) scheduled for launch from KSC late in 1967,
11900-416: The Saturn V launched Apollo 11 , putting the first men on the Moon. The size and payload capacity of the Saturn V dwarfed those of all other previous rockets successfully flown at that time. With the Apollo spacecraft on top, it stood 363 feet (111 m) tall, and, ignoring the fins, was 33 feet (10 m) in diameter. Fully fueled, the Saturn V weighed 6.5 million pounds (2,900,000 kg) and had
12070-434: The Saturn V second stage S-II-T ruptured during pressure tests at SSC on 28 May 1966, and five North American Aviation technicians monitoring the test received minor injuries. The accident occurred when the hydrogen fuel tank failed under pressure. S-II-T, which had five hydrogen-oxygen J-2 engines capable of generating one million pounds of thrust, had been tested May 25 in ground firing but stopped firing after 195 seconds when
12240-615: The Saturn V shared characteristics with the one carried by the Saturn IB. The Saturn V was primarily constructed of aluminum . It was also made of titanium , polyurethane , cork and asbestos . Blueprints and other plans of the rocket are available on microfilm at the Marshall Space Flight Center. The Saturn V consisted of three stages—the S-IC first stage, S-II second stage, and S-IVB third stage—and
12410-627: The Saturn ;V. The C-1 became the Saturn I and C-1B became Saturn IB. Von Braun headed a team at the MSFC to build a vehicle capable of launching a crewed spacecraft to the Moon. During these revisions, the team rejected the single engine of the V-2's design and moved to a multiple-engine design. The Saturn V's final design had several key features. F-1 engines were chosen for the first stage, while new liquid hydrogen propulsion system called J-2 for
12580-422: The Solar System. Mars has long been a planet of intense fascination for NASA, being suspected of potentially having harbored life. Mariner 5 was the first NASA spacecraft to flyby Mars, followed by Mariner 6 and Mariner 7 . Mariner 9 was the first orbital mission to Mars. Launched in 1975, Viking program consisted of two landings on Mars in 1976. Follow-on missions would not be launched until 1996, with
12750-649: The Soviets. They turned to von Braun's team, who had created the Jupiter series of rockets . The Juno I rocket launched the first American satellite in January 1958. Von Braun considered the Jupiter series of rockets to be a prototype of the upcoming Saturn series of rockets , and referred to it as "an infant Saturn". Named after the sixth planet from the Sun , the design of the various Saturn rockets evolved from
12920-633: The Space Shuttle Columbia disaster in 2003, NASA was forced to rely on Russian Soyuz launches for its astronauts and the 2011 retirement of the Space Shuttle accelerated the station's completion. In the 1980s, right after the first flight of the Space Shuttle, NASA started a joint program with the Department of Defense to develop the Rockwell X-30 National Aerospace Plane. NASA realized that
13090-418: The Space Shuttle allowed NASA to begin recruiting more non-military scientific and technical experts. A prime example is Sally Ride , who became the first American woman to fly in space on STS-7 . This new astronaut selection process also allowed NASA to accept exchange astronauts from U.S. allies and partners for the first time. The first Space Shuttle flight occurred in 1981, when the Columbia launched on
13260-514: The Space Shuttle and expand space exploration beyond low Earth orbit. Constellation was intended to use a significant amount of former Space Shuttle equipment and return astronauts to the Moon. This program was canceled by the Obama Administration . Former astronauts Neil Armstrong , Gene Cernan , and Jim Lovell sent a letter to President Barack Obama to warn him that if the United States did not get new human spaceflight ability,
13430-554: The Space Shuttle began flying, selling it as an orbital laboratory, repair station, and a jumping off point for lunar and Mars missions. NASA found a strong advocate in President Ronald Reagan , who declared in a 1984 speech: America has always been greatest when we dared to be great. We can reach for greatness again. We can follow our dreams to distant stars, living and working in space for peaceful, economic, and scientific gain. Tonight I am directing NASA to develop
13600-686: The Space Shuttle, while a massive technological accomplishment, would not be able to live up to all its promises. Designed to be a single-stage-to-orbit spaceplane, the X-30 had both civil and military applications. With the end of the Cold War , the X-30 was canceled in 1992 before reaching flight status. Following the Space Shuttle Columbia disaster in 2003, President Bush started the Constellation program to smoothly replace
13770-483: The Space Shuttle. Due to technical challenges, the spacecraft was cancelled in 2001. Despite this, it was the first time a commercial space company directly expended a significant amount of its resources into spacecraft development. The advent of space tourism also forced NASA to challenge its assumption that only governments would have people in space. The first space tourist was Dennis Tito , an American investment manager and former aerospace engineer who contracted with
13940-580: The Space Station Freedom was controversial, with much of the debate centering on cost. Several redesigns to reduce cost were conducted in the early 1990s, stripping away much of its functions. Despite calls for Congress to terminate the program, it continued, in large part because by 1992 it had created 75,000 jobs across 39 states. By 1993, President Bill Clinton attempted to significantly reduce NASA's budget and directed costs be significantly reduced, aerospace industry jobs were not lost, and
14110-513: The SpaceX funding commitment to the methane modification project has not yet been disclosed, as the contract has not yet been finalized and executed. The methane modifications will become a permanent part of the Stennis test infrastructure and will be available to other users of the test facility after the SpaceX facility lease is completed. As of October 2013, the most recent test completed on
14280-602: The U.S. risked become a second or third-rate space power. As early as the Reagan Administration, there had been calls for NASA to expand private sector involvement in space exploration rather than do it all in-house. In the 1990s, NASA and Lockheed Martin entered into an agreement to develop the Lockheed Martin X-33 demonstrator of the VentureStar spaceplane, which was intended to replace
14450-474: The United States at that time. Two main reasons for the cancellation of the last three Apollo missions were the heavy investments in Saturn V and the ever-increasing costs of the Vietnam War to the U.S. in money and resources. In the time frame from 1969 to 1971 the cost of launching a Saturn V Apollo mission was between $ 185,000,000 to $ 189,000,000, of which $ 110 million were used for the production of
14620-678: The United States' military and civil spaceflight programs, which were organized together under the Defense Department 's Advanced Research Projects Agency . NASA was established on July 29, 1958, with the signing of the National Aeronautics and Space Act and it began operations on October 1, 1958. As the US's premier aeronautics agency, NACA formed the core of NASA's new structure by reassigning 8,000 employees and three major research laboratories. NASA also proceeded to absorb
14790-535: The acceleration and vehicle attitude , it could calculate the position and velocity of the rocket and correct for any deviations. After the construction and ground testing of each stage was completed, they were each shipped to the Kennedy Space Center. The first two stages were so massive that the only way to transport them was by barge. The S-IC, constructed in New Orleans, was transported down
14960-418: The early stages of launch. If the first stage had used LH2, the volume required would have been more than three times greater, which would have been aerodynamically infeasible at the time. The upper stages also used small solid-propellant ullage motors that helped to separate the stages during the launch, and to ensure that the liquid propellants were in a proper position to be drawn into the pumps. The S-IC
15130-574: The end of the 1960s and installed James E. Webb as NASA administrator to achieve this goal. On May 25, 1961, President Kennedy openly declared this goal in his "Urgent National Needs" speech to the United States Congress, declaring: I believe this Nation should commit itself to achieving the goal, before this decade is out, of landing a man on the Moon and returning him safely to Earth. No single space project in this period will be more impressive to mankind, or more important for
15300-464: The end of the Apollo program in the early 1970s. It was announced in 1971 that the center would be performing tests on the engines for the new Space Shuttle program (called the SSME ). The A-1 and A-2 test stands, originally designed to accommodate the physically much larger S-II J-2 engines, were modified to accept the smaller SSME, and testing officially began on May 19, 1975, when the first such engine
15470-510: The engines are designed eventually to launch the biconic-shaped Space Vehicle the company is developing. On 22 May 2014, an AJ26 rocket engine under test on the Stennis E-1 test stand, for a future Orbital Sciences Antares launch, failed and caused major damage to the E-1 test stand. As of 10 June, neither NASA, Orbital, nor Aerojet Rocketdyne have released any additional information on
15640-605: The entire stack was moved from the Vehicle Assembly Building (VAB) to the launch pad using the Crawler Transporter (CT). Built by the Marion Power Shovel Company (and later used for transporting the smaller and lighter Space Shuttle, as well as the Space Launch System ), the CT ran on four double-tracked treads, each with 57 "shoes". Each shoe weighed 2,000 pounds (910 kg). This transporter
15810-446: The extent of the damage, nor time frame when the three test cells in the E-1 test stand will return to operational status. As of early June 2014, the E-1 test stand was non-operational pending the completion of an investigation into a rocket engine failure on the test stand on 22 May 2014. In June 2015, Aerojet Rocketdyne signed a contract with NASA to upgrade the E-1 test stand so that the "multi-element pre-burner and main injector" of
15980-417: The first 30 seconds of flight. If all three stages were to explode simultaneously on the launch pad, an unlikely event, the Saturn V had a total explosive yield of 543 tons of TNT or 0.543 kilotons (2,271,912,000,000 J or 155,143 lbs of weight loss), which is 0.222 kt for the first stage, 0.263 kt for the second stage and 0.068 kt for the third stage. (See Saturn V Instrument Unit ) Contrary to popular myth ,
16150-496: The first MTF S-IC firing, proved the total compatibility of stage, mechanical support equipment, and S-IC test facilities. A second S-IC-T firing lasted for 60 seconds on March 17, 1967. This firing validated the flame-bucket-water-flow pattern of the B-2 test stand and ended the facilities checkout test series at MTF. Boeing personnel removed the S-IC-T from test stand B-2 on March 24, 1967, following post-static checkout, test stand refurbishment, and facilities modification. During
16320-458: The first and second stages of the Saturn V rockets. The facility was renamed again to Mississippi Test Facility on July 1, 1965, became a part of the Marshall Space Flight Center . Starting in 1971, all Space Shuttle Main Engines were flight-certified at Stennis. On June 14, 1974, the site was renamed National Space Technology Laboratories , a name that continued until May 20, 1988, when it
16490-420: The first close up view of the planet. Both probes became the first objects to leave the Solar System. The Voyager program launched in 1977, conducting flybys of Jupiter and Saturn , Neptune , and Uranus on a trajectory to leave the Solar System. The Galileo spacecraft, deployed from the Space Shuttle flight STS-34 , was the first spacecraft to orbit Jupiter, discovering evidence of subsurface oceans on
16660-515: The first crew to make it habitable and operational. Skylab hosted nine missions and was decommissioned in 1974 and deorbited in 1979, two years prior to the first launch of the Space Shuttle and any possibility of boosting its orbit. In 1975, the Apollo–Soyuz mission was the first ever international spaceflight and a major diplomatic accomplishment between the Cold War rivals, which also marked
16830-402: The first humans to see the Earth as a globe in space, the first to witness an Earthrise , and the first to see and manually photograph the far side of the Moon. The first lunar landing was conducted by Apollo 11. Commanded by Neil Armstrong with astronauts Buzz Aldrin and Michael Collins , Apollo 11 was one of the most significant missions in NASA's history, marking the end of
17000-616: The first operational use of the A-2 stand. The first full-duration firing of the S-II flight stage occurred 20 May 1966 when S-II-T test-fired on the A-2 test stand for 354.5 seconds. LOX cutoff sensors initiated cutoff automatically. The firing passed all major test objectives with the exception of the propellant utilization system. This was the fourth static firing of the S-II-T. The stage developed one million pounds of thrust from its five hydrogen-oxygen-powered J-2 engines. A static test version of
17170-467: The first quarter of fiscal year 2002. The facility was to be used to evaluate beam quality, efficiency, and power levels for a prototype megawatt-class hydrogen fluoride laser. NASA The National Aeronautics and Space Administration ( NASA / ˈ n æ s ə / ) is an independent agency of the U.S. federal government responsible for the civil space program , aeronautics research, and space research. Established in 1958 , it succeeded
17340-457: The first stage ignition sequence started. The center engine ignited first, followed by opposing outboard pairs at 300-millisecond intervals to reduce the structural loads on the rocket. When thrust had been confirmed by the onboard computers, the rocket was "soft-released" in two stages: first, the hold-down arms released the rocket, and second, as the rocket began to accelerate upwards, it was slowed by tapered metal pins pulled through holes for half
17510-560: The first such test occurring on December 18, 2007. Stennis tested Aerojet Rocketdyne AJ26 rocket engines for Orbital Sciences Corp. of Dulles, Va., which partnered with NASA to provide commercial cargo flights to the International Space Station. Orbital's maiden flight to the space station launched from NASA's Wallops Flight Facility in Virginia September 18, 2013. Orbital's Antares rocket was powered by
17680-426: The five J-2 engines. For the first seven crewed Apollo missions, only four ullage motors were used on the S-II, and they were eliminated for the final four launches. About 30 seconds after first stage separation, the interstage ring dropped from the second stage. This was done with an inertially fixed attitude—orientation around its center of gravity —so that the interstage, only 3 feet 3 inches (1 m) from
17850-416: The four outer engines for control. The S-II was 81.6 feet (24.87 m) tall with a diameter of 33 feet (10 m), identical to the S-IC, and thus was the largest cryogenic stage until the launch of the Space Shuttle in 1981. The S-II had a dry mass of about 80,000 pounds (36,000 kg); when fully fueled, it weighed 1,060,000 pounds (480,000 kg). The second stage accelerated the Saturn V through
18020-433: The hypersonic test aircraft becoming the first non-dedicated spacecraft to cross from the atmosphere to outer space. The X-15 also served as a testbed for Apollo program technologies, as well as ramjet and scramjet propulsion. Escalations in the Cold War between the United States and Soviet Union prompted President John F. Kennedy to charge NASA with landing an American on the Moon and returning him safely to Earth by
18190-451: The last flight of the Apollo capsule. Flown in 1975, a U.S. Apollo spacecraft docked with a Soviet Soyuz capsule. During the 1960s, NASA started its space science and interplanetary probe program. The Mariner program was its flagship program, launching probes to Venus , Mars , and Mercury in the 1960s. The Jet Propulsion Laboratory was the lead NASA center for robotic interplanetary exploration, making significant discoveries about
18360-449: The liquid hydrogen pressure sensors and switches had been disconnected, had attempted to pressurize the tank. Believing that a liquid hydrogen vent valve was leaking, the technicians closed the facility by blocking valves. This had caused the vehicle tank to become over-pressurized and burst. On 30 May 1966 the board released its findings after two days of inquiry. The fuel tank of the S-II stage had been pressurized beyond design limits. There
18530-484: The long-range exploration of space; and none will be so difficult or expensive to accomplish. Kennedy gave his " We choose to go to the Moon " speech the next year, on September 12, 1962 at Rice University , where he addressed the nation hoping to reinforce public support for the Apollo program. Despite attacks on the goal of landing astronauts on the Moon from the former president Dwight Eisenhower and 1964 presidential candidate Barry Goldwater , President Kennedy
18700-434: The majority of the International Space Station, Russia, Canada, Japan, and the European Space Agency all contributed components. Despite NASA's insistence that costs would be kept at a budget of $ 17.4, they kept rising and NASA had to transfer funds from other programs to keep the International Space Station solvent. Ultimately, the total cost of the station was $ 150 billion, with the United States paying for two-thirds.Following
18870-556: The military. The Mercury 7 astronauts included three Air Force pilots, three Navy aviators, and one Marine Corps pilot. On May 5, 1961, Alan Shepard became the first American to enter space, performing a suborbital spaceflight in the Freedom 7 . This flight occurred less than a month after the Soviet Yuri Gagarin became the first human in space, executing a full orbital spaceflight. NASA's first orbital spaceflight
19040-634: The moon of Enceladus , which could harbor life. Finally launched in 2006, the New Horizons mission was the first spacecraft to visit Pluto and the Kuiper Belt . Beyond interplanetary probes, NASA has launched many space telescopes . Launched in the 1960s, the Orbiting Astronomical Observatory were NASA's first orbital telescopes, providing ultraviolet, gamma-ray, x-ray, and infrared observations. NASA launched
19210-459: The most fuel-efficient trajectory toward its target orbit. If the instrument unit failed, the crew could switch control of the Saturn to the command module's computer, take manual control, or abort the flight. About 90 seconds before the second stage cutoff, the center engine shut down to reduce longitudinal pogo oscillations. At around this time, the LOX flow rate decreased, changing the mix ratio of
19380-445: The newly redesigned RS-25 engine was completed December 14, 2022. The B-1/B-2 test stand is a dual-position, vertical, static-firing stand supporting a maximum dynamic load of 11M lbf. It was originally built in the 1960s to simultaneously test the five F-1 engines of a complete Saturn-V S1-C first stage from 1967 to 1970. On October 17, 1966, MSFC shipped its S-IC all-system test booster, S-IC-T , to SSC for use in checkout of
19550-476: The next forty years, NACA would conduct aeronautical research in support of the U.S. Air Force , U.S. Army , U.S. Navy , and the civil aviation sector. After the end of World War II , NACA became interested in the possibilities of guided missiles and supersonic aircraft, developing and testing the Bell X-1 in a joint program with the U.S. Air Force . NACA's interest in space grew out of its rocketry program at
19720-500: The noise produced was not able to melt concrete . It took about 12 seconds for the rocket to clear the tower. During this time, it yawed 1.25 degrees away from the tower to ensure adequate clearance despite adverse winds; this yaw, although small, can be seen in launch photos taken from the east or west. At an altitude of 430 feet (130 m) the rocket rolled to the correct flight azimuth and then gradually pitched down until 38 seconds after second stage ignition. This pitch program
19890-411: The northern portion of a sixth ( Pearlington ), and a combined population of 700 families had to be completely relocated off the facility. The effort acquired more than 3,200 parcels of privately owned land – 786 residences, 16 churches, 19 stores, three schools and a wide assortment of commercial buildings, including nightclubs and community centers. Remnants of the communities, including city streets and
20060-821: The original three test stands at Stennis Space Center, the A-1 and A-2 stands were built to test and flight-certify the second stage of the Saturn V , the S-II (pronounced "ess two"), the launch vehicle for the Apollo program . The two stands are similar steel and concrete structures are roughly 200 ft (61 m) tall, and capable of withstanding thrust loads of more than 1 million pounds and temperature of up to 6,000 °F (3,320 °C ). Each test stand can provide Liquid Hydrogen (LH2) and liquid oxygen (LOX) in addition to support fluids, gaseous helium (GHe), gaseous hydrogen (GH2) and gaseous nitrogen (GN2) as purge or pressurizing gasses. Construction began in 1963 and
20230-503: The outboard J-2 engines, would fall cleanly without hitting them, as the interstage could have potentially damaged two of the J-2 engines if it was attached to the S-IC. Shortly after interstage separation the Launch Escape System was also jettisoned. About 38 seconds after the second stage ignition, the Saturn V switched from a preprogrammed trajectory to a "closed loop" or Iterative Guidance Mode. The instrument unit now computed in real time
20400-433: The planning process, NASA considered three methods for the Moon mission: Earth orbit rendezvous (EOR), direct ascent , and lunar orbit rendezvous (LOR). A direct ascent configuration would require an extremely large rocket to send a three-man spacecraft to land directly on the lunar surface. An EOR would launch the direct-landing spacecraft in two smaller parts which would combine in Earth orbit. A LOR mission would involve
20570-551: The powerful F-1 and J-2 rocket engines ; during testing at Stennis Space Center, the force developed by the engines shattered the windows of nearby houses. Designers decided early on to attempt to use as much technology from the Saturn I program as possible for the Saturn V. Consequently, the S-IVB -500 third stage of the Saturn V was based on the S-IVB-200 second stage of the Saturn IB . The instrument unit that controlled
20740-552: The project director of the Saturn V rocket program in August 1963. He developed the requirements for the rocket system and the mission plan for the Apollo program. The first Saturn V launch lifted off from Kennedy Space Center and performed flawlessly on November 9, 1967, Rudolph's birthday. He was then assigned as the special assistant to the director of MSFC in May 1968 and subsequently retired from NASA on January 1, 1969. On July 16, 1969,
20910-625: The radiation levels on Mars were equal to those on the International Space Station , greatly increasing the possibility of Human exploration, and observed the key chemical ingredients for life to occur. In 2013, the Mars Atmosphere and Volatile Evolution ( MAVEN ) mission observed the Martian upper atmosphere and space environment and in 2018, the Interior exploration using Seismic Investigations Geodesy, and Heat Transport ( InSight ) studied
21080-505: The recording of about 800 measurements of the stage's performance, including propellant tank temperatures, engine temperatures, propellant flow rates, and vibrations. On December 30, 1966, MSFC technicians at the MTF test stand conducted a static firing of the first flight version of the Saturn V second stage, S-II-1. This second test firing, like an earlier firing, lasted more than six minutes. On January 11, 1967, initial post-static checkout of
21250-511: The rocket rapidly lost mass, total acceleration including gravity increased to nearly 4 g at T+135 seconds. At this point, the inboard (center) engine was shut down to prevent acceleration from increasing beyond 4 g . When oxidizer or fuel depletion was sensed in the suction assemblies, the remaining four outboard engines were shut down. First stage separation occurred a little less than one second after this to allow for F-1 thrust tail-off. Eight small solid fuel separation motors backed
21420-400: The same height and mass and contained the same electrical connections as the actual stages. NASA stacked (assembled) the Saturn V on a Mobile Launcher , which consisted of a Launch Umbilical Tower with nine swing arms (including the crew access arm), a "hammerhead" crane, and a water suppression system which was activated prior to engine ignition during a launch. After assembly was completed,
21590-507: The satellites were repaired and relaunched. Despite ushering in a new era of spaceflight, where NASA was contracting launch services to commercial companies, the Space Shuttle was criticized for not being as reusable and cost-effective as advertised. In 1986, Challenger disaster on the STS-51L mission resulted in the loss of the spacecraft and all seven astronauts on launch, grounding the entire space shuttle fleet for 36 months and forced
21760-469: The second and third stage. NASA had finalized its plans to proceed with von Braun's Saturn designs, and the Apollo space program gained speed. The stages were designed by von Braun's Marshall Space Flight Center in Huntsville, and outside contractors were chosen for the construction: Boeing ( S-IC ), North American Aviation ( S-II ), Douglas Aircraft ( S-IVB ), and IBM ( instrument unit ). Early in
21930-676: The separation of dark and regular matter during galactic collisions. Finally, the Spitzer Space Telescope is an infrared telescope launched in 2003 from a Delta II rocket. It is in a trailing orbit around the Sun, following the Earth and discovered the existence of brown dwarf stars . Other telescopes, such as the Cosmic Background Explorer and the Wilkinson Microwave Anisotropy Probe , provided evidence to support
22100-508: The setback caused by the Apollo 1 fire, which killed three astronauts, the program proceeded. Apollo 8 was the first crewed spacecraft to leave low Earth orbit and the first human spaceflight to reach the Moon . The crew orbited the Moon ten times on December 24 and 25, 1968, and then traveled safely back to Earth . The three Apollo 8 astronauts— Frank Borman , James Lovell , and William Anders —were
22270-527: The shaped explosive charges attached to the outer surfaces of the rocket to detonate. These would make cuts in fuel and oxidizer tanks to disperse the fuel quickly and to minimize mixing. The pause between these two actions would give time for the crew to escape via the Launch Escape Tower or (in the later stages of the flight) the propulsion system of the Service module. A third command, "safe",
22440-595: The shuttle era it was modified to test the Space Shuttle Main Engine (SSME). Stennis now leases the B-1 test position to Pratt & Whitney Rocketdyne for testing of RS-68 engines for the Delta IV launch vehicle. NASA has prepared the B-2 test position to test the core stage of NASA's Space Launch System (SLS), which it first did in early 2021. The SLS Core Stage, with four RS-25D rocket engines,
22610-613: The site to be located between the rockets' manufacturing facility at Michoud Assembly Facility in eastern New Orleans, Louisiana , and the launch facility at the Kennedy Space Center in Florida. Also, the site required barge access as the rocket stages to be tested for Apollo were too large for overland transport. Additionally, the Apollo motors were too loud to be tested at Marshall Space Flight Center 's existing test stands near Huntsville, Alabama . A more isolated site
22780-592: The space agency where he would serve as the director of the Apollo program. Development of the Saturn V rocket was led by Wernher von Braun and his team at the Marshall Space Flight Center , derived from the Army Ballistic Missile Agency's original Saturn I . The Apollo spacecraft was designed and built by North American Aviation , while the Apollo Lunar Module was designed and built by Grumman . To develop
22950-549: The space shuttle be retired. In 2006, the Space Shuttle returned to flight, conducting several mission to service the Hubble Space Telescope , but was retired following the STS-135 resupply mission to the International Space Station in 2011. NASA never gave up on the idea of a space station after Skylab's reentry in 1979. The agency began lobbying politicians to support building a larger space station as soon as
23120-481: The space station spelled an end to the program. In 2003, a second space shuttle was destroyed when the Columbia was destroyed upon reentry during the STS-107 mission, resulting in the loss of the spacecraft and all seven astronauts. This accident marked the beginning of the retiring of the Space Shuttle program, with President George W. Bush directing that upon the completion of the International Space Station,
23290-466: The spaceflight skills and equipment required for a lunar mission, NASA initiated Project Gemini . Using a modified Air Force Titan II launch vehicle, the Gemini capsule could hold two astronauts for flights of over two weeks. Gemini pioneered the use of fuel cells instead of batteries, and conducted the first American spacewalks and rendezvous operations . The Ranger Program was started in
23460-462: The stage into the S-II stage service and checkout building for inspection and preparation for static firing. On December 1, 1966, North American Aviation conducted a successful 384-second captive firing of five J-2 engines, the first flight hydrogen-fueled engines, developing a total one million pounds of thrust. During the test, number 2 and 4 engine SLAM arms did not drop, resulting in the successful gimballing of engines 1 and 3 only. The test included
23630-534: The stand is expected to be unused after its completion. The A-3 stand may however, be able to be refurnished to test a new mission when needed. In 2014, journalists writing for Bloomberg News and the Washington Times criticized the continued construction work on the $ 350 million test stand, and characterized it as a wasteful earmark by Mississippi U.S. senator Roger F. Wicker . American-New Zealand launch service provider Rocket Lab intends to use
23800-522: The test stand began immediately. Static firing would occur in early 1967 to demonstrate the facility checkout system. On 13 February 1967 Corps of Engineers personnel completed construction of the S-IC B-2 test stand at MTF. Following an extensive systems, subsystems, and total integrated systems checkout of the B-2 test stand at MTF on March 3, 1967, workmen successfully fired the S-IC battleship/all-systems stage (S-IC-T) for 15 seconds. This S-IC-T test,
23970-458: The top of the LOX tank and bottom of the LH2 tank. It consisted of two aluminum sheets separated by a honeycomb structure made of phenolic resin . This bulkhead had to be able to insulate against the 126 °F (70 °C) temperature difference between the two tanks. The use of a common bulkhead saved 7,900 pounds (3.6 t) by both eliminating one bulkhead and reducing the stage's length. Like
24140-465: The two launch pads). From 1964 until 1973, $ 6.417 billion (equivalent to $ 40.9 billion in 2023) was appropriated for the Research and Development and flights of the Saturn V, with the maximum being in 1966 with $ 1.2 billion (equivalent to $ 8.61 billion in 2023). That same year, NASA received its largest total budget of $ 4.5 billion, about 0.5 percent of the gross domestic product (GDP) of
24310-439: The two propellants and ensuring that there would be as little propellant as possible left in the tanks at the end of second stage flight. This was done at a predetermined delta-v . Five level sensors in the bottom of each S-II propellant tank were armed during S-II flight, allowing any two to trigger S-II cutoff and staging when they were uncovered. One second after the second stage cut off it separated and several seconds later
24480-422: The upper atmosphere with 1,100,000 pounds-force (4,900 kN) of thrust in a vacuum. When loaded with fuel, more than 90 percent of the mass of the stage was propellant; however, the ultra-lightweight design had led to two failures in structural testing. Instead of having an intertank structure to separate the two fuel tanks as was done in the S-IC, the S-II used a common bulkhead that was constructed from both
24650-412: The various projects, mission architectures and associated timelines relevant to lunar and Mars exploration and science. Saturn V The Saturn V is a retired American super heavy-lift launch vehicle developed by NASA under the Apollo program for human exploration of the Moon . The rocket was human-rated , had three stages , and was powered by liquid fuel . Flown from 1967 to 1973, it
24820-562: The vehicle (equivalent to $ 1.18 billion–$ 1.2 billion in 2023). The Saturn V carried all Apollo lunar missions, which were launched from Launch Complex 39 at the John F. Kennedy Space Center in Florida . After the rocket cleared the launch tower, flight control transferred to Mission Control at the Johnson Space Center in Houston, Texas . An average mission used the rocket for
24990-461: Was Venus , sharing many similar characteristics to Earth. First visited by American Mariner 2 spacecraft, Venus was observed to be a hot and inhospitable planet. Follow-on missions included the Pioneer Venus project in the 1970s and Magellan , which performed radar mapping of Venus' surface in the 1980s and 1990s. Future missions were flybys of Venus, on their way to other destinations in
25160-440: Was a need for tighter controls over MTF test procedure. Following the destruction of S-II-T, NASA extended the S-II battleship program until July 1967. S-II-1, the first flight S-II stage scheduled for static firing at MTF, left Seal Beach on July 31, 1966. The first flight model (S-II-1) of the Saturn V vehicle's second stage arrived August 13, 1966 at MTF completing its 4,000-mile voyage from Seal Beach. Workmen immediately moved
25330-683: Was able to previously accomplish. NASA launched its first commercial satellites on the STS-5 mission and in 1984, the STS-41-C mission conducted the world's first on-orbit satellite servicing mission when the Challenger captured and repaired the malfunctioning Solar Maximum Mission satellite. It also had the capability to return malfunctioning satellite to Earth, like it did with the Palapa B2 and Westar 6 satellites. Once returned to Earth,
25500-424: Was able to protect NASA's growing budget, of which 50% went directly to human spaceflight and it was later estimated that, at its height, 5% of Americans worked on some aspect of the Apollo program. Mirroring the Department of Defense's program management concept using redundant systems in building the first intercontinental ballistic missiles, NASA requested the Air Force assign Major General Samuel C. Phillips to
25670-472: Was also a concern with sharing sensitive space technologies with the Europeans, which had the potential to dilute America's technical lead. Ultimately, an international agreement to develop the Space Station Freedom program would be signed with thirteen countries in 1985, including the European Space Agency member states, Canada , and Japan . Despite its status as the first international space program,
25840-471: Was also designed with high mass efficiency, though not quite as aggressively as the S-II. The S-IVB had a dry mass of about 23,000 pounds (10,000 kg) and, when fully fueled, weighed about 262,000 pounds (119,000 kg). The S-IVB was the only rocket stage of the Saturn V small enough to be transported by the cargo plane Aero Spacelines Pregnant Guppy . For lunar missions it was fired twice: first for Earth orbit insertion after second stage cutoff, and
26010-585: Was also required to keep the rocket level as it traveled the 3 miles (4.8 km) to the launch site, especially at the 3 percent grade encountered at the launch pad. The CT also carried the Mobile Service Structure (MSS), which allowed technicians access to the rocket until eight hours before launch, when it was moved to the "halfway" point on the Crawlerway (the junction between the VAB and
26180-573: Was built by the Boeing Company at the Michoud Assembly Facility , New Orleans , where the Space Shuttle external tanks would later be built by Lockheed Martin . Most of its mass at launch was propellant: RP-1 fuel with liquid oxygen as the oxidizer . The stage was 138 feet (42 m) tall and 33 feet (10 m) in diameter. It provided 7,750,000 lbf (34,500 kN) of thrust at sea level. The S-IC stage had
26350-403: Was carried by the Aero Spacelines Pregnant Guppy and Super Guppy , but could also have been carried by barge if warranted. Upon arrival at the Vertical Assembly Building, each stage was inspected in a horizontal position before being oriented vertically. NASA also constructed large spool-shaped structures that could be used in place of stages if a particular stage was delayed. These spools had
26520-445: Was conducted by John Glenn on February 20, 1962, in the Friendship 7 , making three full orbits before reentering. Glenn had to fly parts of his final two orbits manually due to an autopilot malfunction. The sixth and final Mercury mission was flown by Gordon Cooper in May 1963, performing 22 orbits over 34 hours in the Faith 7 . The Mercury Program was wildly recognized as a resounding success, achieving its objectives to orbit
26690-429: Was designed to accommodate up to 500,000 pounds-force (2,224 kN) engines and powerpack systems testing in a horizontal configuration. The E4 test stand was proposed in the year 2000 to be located near the H1 test stand. In 2001, the Pentagon's Ballistic Missile Defense Organization proposed construction of a $ 140 million facility at Stennis H-1 test stand to test its proposed Space-Based Laser (SBL) to begin in
26860-571: Was finished in 1966. The A Test Complex also includes a Test Control Center, observation bunkers, and various technical and support systems. On 23 April 1966 workmen at the A-2 test stand successfully captive-fired for 15 seconds the S-II-T, Structural and Dynamic Test Vehicle for the Saturn V second stage, in an all-systems test. This was the first test of a flight-weight S-II stage. The stage, largest and most powerful liquid oxygen-liquid hydrogen stage known, developed one million pounds of thrust from its five Rocketdyne J-2 engines. This test also marked
27030-400: Was installed on the stand for propellant fill and drain testing and two hot-fire tests. In August 2007, NASA began construction of the A-3 test stand at SSC. The A-3 stand was to be used for testing J-2X engines under vacuum conditions simulating high altitude operation. A-3 will also be operable as a sea-level test facility. However, because the Constellation Program was cancelled in 2010,
27200-442: Was launched in 1990 on STS-31 from the Discovery and could view galaxies 15 billion light years away. A major defect in the telescope's mirror could have crippled the program, had NASA not used computer enhancement to compensate for the imperfection and launched five Space Shuttle servicing flights to replace the damaged components. The Compton Gamma Ray Observatory was launched from the Atlantis on STS-37 in 1991, discovering
27370-436: Was needed. After an exhaustive site selection process that included reviews of other coastal locations including Eglin Air Force Base in Florida plus islands in both the Caribbean and the Pacific, NASA announced formation of the Mississippi Test Facility (now known as Stennis Space Center) on Oct. 25, 1961, for testing engines for the Apollo Program. A high-terrace area bordering the East Pearl River in Hancock County, Miss.,
27540-433: Was renamed for Mississippi senator and space program supporter John C. Stennis . With the end of the Apollo and Shuttle programs, use of the base decreased, with economic impact to the surrounding communities. Over the years, other government organizations and commercial entities have moved to and left from the facility, in the balance providing a major economic benefit to the communities. The Rocket Propulsion Test Complex
27710-412: Was scheduled for testing at MTF late in March 1967. On February 17, 1967, the first full-duration test of a cluster of uprated J-2 engines, S-II battleship test No. 041, lasted 360 seconds. On February 25, 1967, workmen completed construction of the S-II A-1 test stand, and the Corps of Engineers accepted beneficial occupancy with exceptions. On March 17, 1967, technicians fired the S-II battleship stage for
27880-413: Was selected for its location. NASA entrusted the U.S. Army Corps of Engineers with the difficult task to procure each land parcel either by directly purchasing the land or through acquisition of a perpetual easement. The selected area was thinly populated and met all other requirements; however before construction began, five small communities (Gainesville, Logtown, Napoleon, Santa Rosa, and Westonia), plus
28050-400: Was set according to the prevailing winds during the launch month. The four outboard engines also tilted toward the outside so that in the event of a premature outboard engine shutdown the remaining engines would thrust through the rocket's center of mass . The Saturn V reached 400 feet per second (120 m/s) at over 1 mile (1,600 m) in altitude. Much of the early portion of the flight
28220-451: Was spent gaining altitude, with the required velocity coming later. The Saturn V broke the sound barrier at just over 1 minute at an altitude of between 3.45 and 4.6 miles (5.55 and 7.40 km). At this point, shock collars, or condensation clouds, would form around the bottom of the command module and around the top of the second stage. At about 80 seconds, the rocket experienced maximum dynamic pressure (max q). The dynamic pressure on
28390-413: Was tested on the A-1 stand. The center continued to test engines for the duration of the shuttle program, on the A-1 and A-2 stands with the final scheduled test occurred on July 29, 2009, on the A-2 stand. As the shuttle program is phased out, the A-1 and A-2 test stands are seeing new use testing the next generation of rocket engines, including the J-2X engine designed to power the SLS upper stage, with
28560-427: Was turned off about 26 seconds earlier than the outboard engines to limit acceleration. During launch, the S-IC fired its engines for 168 seconds (ignition occurred about 8.9 seconds before liftoff) and at engine cutoff, the vehicle was at an altitude of about 42 miles (67 km), was downrange about 58 miles (93 km), and was moving around 7,500 feet per second (2,300 m/s). While not put into production,
28730-453: Was used after the S-IVB stage reached orbit to irreversibly deactivate the self-destruct system. The system was also held inactive as long as the rocket was still on the launch pad. The first stage burned for about 2 minutes and 41 seconds, lifting the rocket to an altitude of 42 miles (68 km) and a speed of 6,164 miles per hour (2,756 m/s) and burning 4,700,000 pounds (2,100,000 kg) of propellant. At 8.9 seconds before launch,
28900-452: Was used for nine crewed flights to the Moon, and to launch Skylab , the first American space station . As of 2024, the Saturn V remains the only launch vehicle to have carried humans beyond low Earth orbit (LEO). The Saturn V holds the record for the largest payload capacity to low Earth orbit, 311,152 lb (141,136 kg), which included unburned propellant needed to send the Apollo command and service module and Lunar Module to
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