Misplaced Pages

Rocketplane XP

Article snapshot taken from Wikipedia with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.

Blue Origin NS-22

#131868

60-540: The Rocketplane XP was a suborbital spaceplane design that was under development c. 2005 by Rocketplane Kistler . The vehicle was to be powered by two jet engines and a rocket engine , intended to enable it to reach suborbital space. The XP would have operated from existing spaceports in a manner consistent with established commercial aviation practices. Commercial flights were projected to begin in 2009. Rocketplane Global declared bankruptcy in mid-June 2010. Their assets were auctioned off in 2011. As envisioned,

120-404: A > − μ R {\displaystyle \varepsilon =-{\mu \over {2a}}>-{\mu \over {R}}\,\!} where μ {\displaystyle \mu \,\!} is the standard gravitational parameter . Almost always a < R , corresponding to a lower ϵ {\displaystyle \epsilon } than the minimum for

180-562: A "sub-orbital spaceflight". Usually a rocket is used, but some experimental sub-orbital spaceflights have also been achieved via the use of space guns . By definition, a sub-orbital spaceflight reaches an altitude higher than 100 km (62 mi) above sea level . This altitude, known as the Kármán line, was chosen by the Fédération Aéronautique Internationale because it is roughly the point where

240-461: A LEO. The maximum speed at the lower ends of the trajectory are now composed of a horizontal and a vertical component. The higher the horizontal distance covered, the greater the horizontal speed will be. (The vertical velocity will increase with distance for short distances but will decrease with distance at longer distances.) For the V-2 rocket , just reaching space but with a range of about 330 km,

300-471: A crew of two pilots, to an altitude of 200 km (65,000 ft) using captured V-2 . In 2004, a number of companies worked on vehicles in this class as entrants to the Ansari X Prize competition. The Scaled Composites SpaceShipOne was officially declared by Rick Searfoss to have won the competition on October 4, 2004, after completing two flights within a two-week period. In 2005, Sir Richard Branson of

360-439: A full orbit, which is − μ 2 R {\displaystyle -{\mu \over {2R}}\,\!} Thus the net extra specific energy needed compared to just raising the spacecraft into space is between 0 and μ 2 R {\displaystyle \mu \over {2R}\,\!} . To minimize the required delta-v (an astrodynamical measure which strongly determines

420-498: A halo) centered on the badge's shield, or escutcheon . The United States Air Force and United States Army astronaut badges are issued in three degrees: Basic, senior, and command (Air Force)/master (Army). The senior astronaut badge is denoted by a star centered above the decoration, while the command/master level is indicated by a star and wreath. To earn an astronaut badge, a U.S. Air Force or U.S. Navy and Marine Corps officer must complete all required training and participate in

480-563: A lift off from Texas and a simulated soft touchdown in the Indian Ocean 66 minutes after liftoff. Sub-orbital flights can last from just seconds to days. Pioneer 1 was NASA 's first space probe , intended to reach the Moon . A partial failure caused it to instead follow a sub-orbital trajectory, reentering the Earth's atmosphere 43 hours after launch. To calculate the time of flight for

540-447: A maximum speed of 7 or 8 km/s. The minimum delta-v and the corresponding maximum altitude for a given range can be calculated, d , assuming a spherical Earth of circumference 40 000  km and neglecting the Earth's rotation and atmosphere. Let θ be half the angle that the projectile is to go around the Earth, so in degrees it is 45°× d / 10 000  km . The minimum-delta-v trajectory corresponds to an ellipse with one focus at

600-765: A minimum-delta-v trajectory, according to Kepler's third law , the period for the entire orbit (if it did not go through the Earth) would be: period = ( semi-major axis R ) 3 2 × period of low Earth orbit = ( 1 + sin ⁡ θ 2 ) 3 2 2 π R g {\displaystyle {\text{period}}=\left({\frac {\text{semi-major axis}}{R}}\right)^{\frac {3}{2}}\times {\text{period of low Earth orbit}}=\left({\frac {1+\sin \theta }{2}}\right)^{\frac {3}{2}}2\pi {\sqrt {\frac {R}{g}}}} Using Kepler's second law , we multiply this by

660-478: A quarter of the way around the Earth, and 42 minutes for going halfway around. For short distances, this expression is asymptotic to 2 d / g {\displaystyle {\sqrt {2d/g}}} . From the form involving arccosine, the derivative of the time of flight with respect to d (or θ) goes to zero as d approaches 20 000  km (halfway around the world). The derivative of Δ v also goes to zero here. So if d = 19 000  km ,

SECTION 10

#1732791260132

720-445: A space flight more than 50 miles (80 kilometers) above the Earth. The U.S. Army has awarded the badge to officers that have orbited the Earth. The U.S. Air Force Astronaut Badge consists of a standard USAF aeronautical badge upon which is centered the astronaut device. The Air Force does not consider Astronaut to be a separate rating from its six established rating badges, but as a "qualifier" to them, and may only be awarded by

780-492: A vehicle flying fast enough to support itself with aerodynamic lift from the Earth's atmosphere would be flying faster than orbital speed . The US military and NASA award astronaut wings to those flying above 50 mi (80 km), although the U.S. State Department does not show a distinct boundary between atmospheric flight and spaceflight . During freefall the trajectory is part of an elliptic orbit as given by

840-446: Is a hypersonic suborbital spaceplane concept that could transport 50 passengers from Australia to Europe in 90 minutes or 100 passengers from Europe to California in 60 minutes. The main challenge lies in increasing the reliability of the different components, particularly the engines, in order to make their use for passenger transportation on a daily basis possible. Astronaut Badge United States astronaut badges are

900-423: Is as scientific sounding rockets . Scientific sub-orbital flights began in the 1920s when Robert H. Goddard launched the first liquid fueled rockets, however they did not reach space altitude. In the late 1940s, captured German V-2 ballistic missiles were converted into V-2 sounding rockets which helped lay the foundation for modern sounding rockets. Today there are dozens of different sounding rockets on

960-468: Is defined as a missile that can hit a target at least 5500 km away, and according to the above formula this requires an initial speed of 6.1 km/s. Increasing the speed to 7.9 km/s to attain any point on Earth requires a considerably larger missile because the amount of fuel needed goes up exponentially with delta-v (see Rocket equation ). The initial direction of a minimum-delta-v trajectory points halfway between straight up and straight toward

1020-411: Is issued by the U.S. Army to Army aviators, flight surgeons, and aircrew members that qualify as astronauts. Army astronauts that have yet to fly a mission and have not previously been awarded any aviation badge are awarded the army aviation badge . Once they have flown a mission, they are awarded the astronaut device, which is affixed to the shield of their army aviation badge. The army astronaut device

1080-453: Is issued in two grades, silver and gold, with the silver pin awarded to candidates who have successfully completed astronaut training and the gold pin to astronauts who have flown in space. Astronaut candidates are given the silver pin but are required to purchase the gold pin at a cost of approximately $ 400. The Mercury astronauts were the first to receive the pins. A unique astronaut pin was made for NASA astronaut Deke Slayton in 1967. It

1140-1134: Is maximized (at about 1320 km) for a trajectory going one quarter of the way around the Earth ( 10 000  km ). Longer ranges will have lower apogees in the minimal-delta-v solution. specific kinetic energy at launch = μ R − μ major axis = μ R sin ⁡ θ 1 + sin ⁡ θ {\displaystyle {\text{specific kinetic energy at launch}}={\frac {\mu }{R}}-{\frac {\mu }{\text{major axis}}}={\frac {\mu }{R}}{\frac {\sin \theta }{1+\sin \theta }}} Δ v = speed at launch = 2 μ R sin ⁡ θ 1 + sin ⁡ θ = 2 g R sin ⁡ θ 1 + sin ⁡ θ {\displaystyle \Delta v={\text{speed at launch}}={\sqrt {2{\frac {\mu }{R}}{\frac {\sin \theta }{1+\sin \theta }}}}={\sqrt {2gR{\frac {\sin \theta }{1+\sin \theta }}}}} (where g

1200-425: Is similar to an ICBM. ICBMs have delta-v's somewhat less than orbital; and therefore would be somewhat cheaper than the costs for reaching orbit, but the difference is not large. Due to the high cost of spaceflight, suborbital flights are likely to be initially limited to high value, very high urgency cargo deliveries such as courier flights, military fast-response operations or space tourism . The SpaceLiner

1260-447: Is the acceleration of gravity at the Earth's surface). The Δ v increases with range, leveling off at 7.9 km/s as the range approaches 20 000  km (halfway around the world). The minimum-delta-v trajectory for going halfway around the world corresponds to a circular orbit just above the surface (of course in reality it would have to be above the atmosphere). See lower for the time of flight. An intercontinental ballistic missile

SECTION 20

#1732791260132

1320-696: The Air Force Chief of Staff after written application upon completion of an operational space mission. The rating of Observer is used for USAF Mission Specialists who have completed training but not a mission and are not otherwise aeronautically rated as a USAF pilot, RPA pilot, combat systems officer, air battle manager, or flight surgeon. In 2007, the U.S. Air Force announced the opening of astronaut mission specialists positions to enlisted personnel who met certain eligibility requirements. These requirements include: No enlisted astronaut badges are yet known to have been issued. The gold astronaut device

1380-491: The Ansari X Prize , horizontal motion is not needed. In this case the lowest required delta-v, to reach 100 km altitude, is about 1.4  km/s . Moving slower, with less free-fall, would require more delta-v. Compare this with orbital spaceflights: a low Earth orbit (LEO), with an altitude of about 300 km, needs a speed around 7.7 km/s, requiring a delta-v of about 9.2 km/s. (If there were no atmospheric drag

1440-470: The Kármán line (about 83 km [52 mi] – 100 km [62 mi] above sea level ), and then falls back to Earth, is considered a sub-orbital spaceflight. Some sub-orbital flights have been undertaken to test spacecraft and launch vehicles later intended for orbital spaceflight . Other vehicles are specifically designed only for sub-orbital flight; examples include crewed vehicles, such as

1500-477: The United States Navy , United States Marine Corps , and United States Coast Guard , with officers of all three branches receiving their designations as aviators or flight officers through the naval aviation flight training program. All three branches also wear the same insignia which consists of naval aviator insignia or naval flight officer insignia with a centered gold astronaut device. However,

1560-656: The Virgin Group announced the creation of Virgin Galactic and his plans for a 9-seat capacity SpaceShipTwo named VSS Enterprise . It has since been completed with eight seats (one pilot, one co-pilot and six passengers) and has taken part in captive-carry tests and with the first mother-ship WhiteKnightTwo , or VMS Eve . It has also completed solitary glides, with the movable tail sections in both fixed and "feathered" configurations. The hybrid rocket motor has been fired multiple times in ground-based test stands, and

1620-596: The X-15 and SpaceShipTwo , and uncrewed ones, such as ICBMs and sounding rockets . Flights which attain sufficient velocity to go into low Earth orbit , and then de-orbit before completing their first full orbit, are not considered sub-orbital. Examples of this include flights of the Fractional Orbital Bombardment System . A flight that does not reach space is still sometimes called sub-orbital, but cannot officially be classified as

1680-730: The X-15 , or the Space Shuttle . Three of the crew members aboard the Ax-1 flight aboard the Crew Dragon Capsule were awarded their civilian astronaut wings by their Mission commander upon becoming the first private citizens to travel to the International Space Station on April 9, 2022. Each of the military services issues its own version of the astronaut badge, which consists of a standard aviation badge with an astronaut device (shooting star through

1740-464: The flight phases before and after the free-fall can vary. For an intercontinental flight the boost phase takes 3 to 5 minutes, the free-fall (midcourse phase) about 25 minutes. For an ICBM the atmospheric reentry phase takes about 2 minutes; this will be longer for any soft landing, such as for a possible future commercial flight. Test flight 4 of the SpaceX 'Starship' performed such a flight with

1800-452: The orbit equation . The perigee distance is less than the radius of the Earth R including atmosphere, hence the ellipse intersects the Earth, and hence the spacecraft will fail to complete an orbit. The major axis is vertical, the semi-major axis a is more than R /2. The specific orbital energy ϵ {\displaystyle \epsilon } is given by: ε = − μ 2

1860-485: The Coast Guard only issues the naval aviator version of the astronaut insignia to its astronauts. NASA issues an astronaut badge to all civilian personnel who qualify as specialists on spaceflight missions. The badge is embroidered in either silver or gold, at the astronaut's discretion, and feature the same astronaut device as the military versions. It is worn on flight suits and flight jackets. A unique badge

Rocketplane XP - Misplaced Pages Continue

1920-636: The International Space Station, and Artemis missions to the moon. The first astronaut pin was created for the Mercury Seven astronauts, in the form of the symbol for the planet Mercury overlaid with the Arabic number "7." As the space program expanded, NASA realized it needed a new symbol to cover personnel on all missions, and created a new lapel pin isolating the "astronaut device" previously applied to flight wings. The pin

1980-654: The Moon on board Apollo 11 in July 1969. Slayton would go on to earn a gold pin in 1975 as a docking module pilot on the Apollo-Soyuz Test Project . A second unique pin was made for Nick Hague after he became the first NASA astronaut to experience an in-flight launch abort . On October 11, 2018, the Soyuz MS-10 mission, part of Expedition 57 to the International Space Station, aborted after one of

2040-524: The Rocketplane XP would carry a pilot and five passengers on a flight profile from a runway using jet engines like a conventional aircraft. It would then climb to about 12 km (40,000 feet). At this point, a reusable rocket engine would power the XP on a suborbital trajectory reaching altitudes of over 100 km (62 mi) after burnout. The XP was to then reenter Earth's atmosphere and land at

2100-638: The United States armed forces. The first astronaut badges were created by taking the astronauts' own aviator badges and overlaying the center shield with a design called the "astronaut device", a star with three trailing rays passing through an ellipse representing orbital flight. In the 1960s, the United States Department of Defense awarded astronaut badges to military and civilian pilots who flew aircraft higher than 50 miles (80 kilometres). Seven USAF and NASA pilots qualified for

2160-437: The XP vehicle. Suborbital A sub-orbital spaceflight is a spaceflight in which the spacecraft reaches outer space , but its trajectory intersects the surface of the gravitating body from which it was launched. Hence, it will not complete one orbital revolution, will not become an artificial satellite nor will it reach escape velocity . For example, the path of an object launched from Earth that reaches

2220-406: The altitude required to qualify as reaching space. The flight path will be either vertical or very steep, with the spacecraft landing back at its take-off site. The spacecraft will shut off its engines well before reaching maximum altitude, and then coast up to its highest point. During a few minutes, from the point when the engines are shut off to the point where the atmosphere begins to slow down

2280-605: The astronaut badge by flying the suborbital X-15 rocket spaceplane. American test pilots Michael Melvill and Brian Binnie were each awarded a commercial astronaut badge by the Federal Aviation Administration (FAA) when they flew sub-orbital missions aboard the Scaled Composites SpaceShipOne rocket spaceplane. All others who have been awarded the astronaut badge earned it travelling to space in non-winged rockets,

2340-439: The centre of the Earth and the other at the point halfway between the launch point and the destination point (somewhere inside the Earth). (This is the orbit that minimizes the semi-major axis, which is equal to the sum of the distances from a point on the orbit to the two foci. Minimizing the semi-major axis minimizes the specific orbital energy and thus the delta-v, which is the speed of launch.) Geometrical arguments lead then to

2400-473: The destination point (which is below the horizon). Again, this is the case if the Earth's rotation is ignored. It is not exactly true for a rotating planet unless the launch takes place at a pole. In a vertical flight of not too high altitudes, the time of the free-fall is both for the upward and for the downward part the maximum speed divided by the acceleration of gravity , so with a maximum speed of 1 km/s together 3 minutes and 20 seconds. The duration of

2460-572: The downward acceleration, the passengers will experience weightlessness . Megaroc had been planned for sub-orbital spaceflight by the British Interplanetary Society in the 1940s. In late 1945, a group led by M. Tikhonravov K. and N. G. Chernysheva at the Soviet NII-4 academy (dedicated to rocket artillery science and technology), began work on a stratospheric rocket project, VR-190 , aimed at vertical flight by

Rocketplane XP - Misplaced Pages Continue

2520-1548: The following (with R being the radius of the Earth, about 6370 km): major axis = ( 1 + sin ⁡ θ ) R {\displaystyle {\text{major axis}}=(1+\sin \theta )R} minor axis = R 2 ( sin ⁡ θ + sin 2 ⁡ θ ) = R sin ⁡ ( θ ) semi-major axis {\displaystyle {\text{minor axis}}=R{\sqrt {2\left(\sin \theta +\sin ^{2}\theta \right)}}={\sqrt {R\sin(\theta ){\text{semi-major axis}}}}} distance of apogee from centre of Earth = R 2 ( 1 + sin ⁡ θ + cos ⁡ θ ) {\displaystyle {\text{distance of apogee from centre of Earth}}={\frac {R}{2}}(1+\sin \theta +\cos \theta )} altitude of apogee above surface = ( sin ⁡ θ 2 − sin 2 ⁡ θ 2 ) R = ( 1 2 sin ⁡ ( θ + π 4 ) − 1 2 ) R {\displaystyle {\text{altitude of apogee above surface}}=\left({\frac {\sin \theta }{2}}-\sin ^{2}{\frac {\theta }{2}}\right)R=\left({\frac {1}{\sqrt {2}}}\sin \left(\theta +{\frac {\pi }{4}}\right)-{\frac {1}{2}}\right)R} The altitude of apogee

2580-513: The four boosters failed to separate properly from the first stage core. The abort happened late enough in the launch sequence that the Soyuz capsule coasted to an apogee of 93 km (58 mi) after separating from the disintegrating rocket. This was above the U.S. definition of the boundary of space at 50 miles (80 km) but below the FAI definition of 100 km (62 mi). In commemoration of his aborted flight, he

2640-475: The length of the minimum-delta-v trajectory will be about 19 500  km , but it will take only a few seconds less time than the trajectory for d = 20 000  km (for which the trajectory is 20 000  km long). While there are a great many possible sub-orbital flight profiles, it is expected that some will be more common than others. The first sub-orbital vehicles which reached space were ballistic missiles . The first ballistic missile to reach space

2700-478: The market, from a variety of suppliers in various countries. Typically, researchers wish to conduct experiments in microgravity or above the atmosphere. Research, such as that done for the X-20 Dyna-Soar project suggests that a semi-ballistic sub-orbital flight could travel from Europe to North America in less than an hour. However, the size of rocket, relative to the payload, necessary to achieve this,

2760-434: The maximum speed is about 7 km/s, and the maximum altitude may be more than 1300 km. Any spaceflight that returns to the surface, including sub-orbital ones, will undergo atmospheric reentry . The speed at the start of the reentry is basically the maximum speed of the flight. The aerodynamic heating caused will vary accordingly: it is much less for a flight with a maximum speed of only 1 km/s than for one with

2820-489: The maximum speed was 1.6 km/s. Scaled Composites SpaceShipTwo which is under development will have a similar free-fall orbit but the announced maximum speed is 1.1 km/s (perhaps because of engine shut-off at a higher altitude). For larger ranges, due to the elliptic orbit the maximum altitude can be much more than for a LEO. On a 10,000-kilometer intercontinental flight, such as that of an intercontinental ballistic missile or possible future commercial spaceflight ,

2880-1946: The portion of the area of the ellipse swept by the line from the centre of the Earth to the projectile: area fraction = 1 π arcsin ⁡ 2 sin ⁡ θ 1 + sin ⁡ θ + 2 cos ⁡ θ sin ⁡ θ π (major axis)(minor axis) {\displaystyle {\text{area fraction}}={\frac {1}{\pi }}\arcsin {\sqrt {\frac {2\sin \theta }{1+\sin \theta }}}+{\frac {2\cos \theta \sin \theta }{\pi {\text{(major axis)(minor axis)}}}}} time of flight = ( ( 1 + sin ⁡ θ 2 ) 3 2 arcsin ⁡ 2 sin ⁡ θ 1 + sin ⁡ θ + 1 2 cos ⁡ θ sin ⁡ θ ) 2 R g = ( ( 1 + sin ⁡ θ 2 ) 3 2 arccos ⁡ cos ⁡ θ 1 + sin ⁡ θ + 1 2 cos ⁡ θ sin ⁡ θ ) 2 R g {\displaystyle {\begin{aligned}{\text{time of flight}}&=\left(\left({\frac {1+\sin \theta }{2}}\right)^{\frac {3}{2}}\arcsin {\sqrt {\frac {2\sin \theta }{1+\sin \theta }}}+{\frac {1}{2}}\cos \theta {\sqrt {\sin \theta }}\right)2{\sqrt {\frac {R}{g}}}\\&=\left(\left({\frac {1+\sin \theta }{2}}\right)^{\frac {3}{2}}\arccos {\frac {\cos \theta }{1+\sin \theta }}+{\frac {1}{2}}\cos \theta {\sqrt {\sin \theta }}\right)2{\sqrt {\frac {R}{g}}}\\\end{aligned}}} This gives about 32 minutes for going

2940-415: The required fuel ), the high-altitude part of the flight is made with the rockets off (this is technically called free-fall even for the upward part of the trajectory). (Compare with Oberth effect .) The maximum speed in a flight is attained at the lowest altitude of this free-fall trajectory, both at the start and at the end of it. If one's goal is simply to "reach space", for example in competing for

3000-455: The same gold pin as veteran astronauts, the diamond was added. The pin was supposed to have been flown on board the Apollo 1 spacecraft , then given to Slayton after the mission was over. However, the Apollo 1 crew died in a fire during a training exercise on January 27, 1967 and the pin was presented to Slayton by the three widows of the dead crew. This diamond-studded gold pin was later flown to

3060-538: The same spaceport under conventional jet power. The relatively low speeds involved meant that heat shielding was not a major concern. The XP was expected to operate from the Clinton-Sherman Industrial Airpark near Burns Flat, Oklahoma . On January 24, 2006 Rocketplane Limited announced a Space Act agreement with NASA Johnson Space Center for the loan of a Rocketdyne RS-88 rocket engine for three years, for use in flight tests of

SECTION 50

#1732791260132

3120-465: The theoretical minimum delta-v would be 8.1 km/s to put a craft into a 300-kilometer high orbit starting from a stationary point like the South Pole. The theoretical minimum can be up to 0.46 km/s less if launching eastward from near the equator.) For sub-orbital spaceflights covering a horizontal distance the maximum speed and required delta-v are in between those of a vertical flight and

3180-532: The various badges of the United States which are awarded to military and civilian personnel of the National Aeronautics and Space Administration , the various child departments of the Department of Defense , or a private space-faring entity , who have performed (or in some cases, completed training for) a spaceflight . The military versions are among the least-awarded qualification badges of

3240-474: Was approved on May 17, 1983. The black version of the device and its sew-on equivalent may be worn on the Army Combat Uniform (ACU); the silver wings with gold device version is authorized for wear on Army Service Uniforms . It is believed to be the rarest badge issued by the U.S. Army. The naval astronaut insignias are issued in a single degree to naval aviators and flight officers from

3300-579: Was created for individuals serving as payload specialists on NASA Space Shuttle missions. Payload specialists were selected by a variety of organizations and included: The payload specialist badge featured a silhouette of the Space Shuttle in place of the astronaut device. In addition to the astronaut badge, which is worn on a military uniform or NASA jumpsuit, astronauts also earn a pin to wear on civilian clothing, signifying their eligibility to take part in missions to space. These include flights to

3360-492: Was fired in a powered flight for the second time on 5 September 2013. Four additional SpaceShipTwos have been ordered and will operate from the new Spaceport America . Commercial flights carrying passengers were expected in 2014, but became cancelled due to the disaster during SS2 PF04 flight . Branson stated, "[w]e are going to learn from what went wrong, discover how we can improve safety and performance and then move forwards together." A major use of sub-orbital vehicles today

3420-413: Was given a pin made of roughly-cast tin . He would later receive a gold pin after his successful mission as part of Expedition 59 / 60 . One silver astronaut pin currently rests on the surface of the Moon, the one that belonged to Clifton Williams , left there by astronaut Alan Bean during Apollo 12 in 1969. Williams was originally scheduled to fly to the Moon as Lunar Module Pilot on Apollo 12 but

3480-455: Was gold in color, like the ones given to astronauts who had flown, and it had a small diamond in place of the star. It was made at the request of the crew of the first crewed mission of the Apollo program as a tribute to Slayton's work at NASA. At the time it was thought that Slayton would never get to space himself, due to a heart condition . Believing that Slayton would refuse to wear exactly

3540-424: Was killed in a plane crash before he was officially assigned to the flight. Bean was his replacement. From 2004 through 2021 the U.S. Federal Aviation Administration created a program to encourage and recognize commercial astronauts , giving special wings to pilots and flight crew on all FAA-licensed commercial flight that exceeded 50 Mile above the surface of the Earth. The FAA Commercial Astronaut Wings design

3600-688: Was the German V-2 , the work of the scientists at Peenemünde , on October 3, 1942, which reached an altitude of 53 miles (85 km). Then in the late 1940s the US and USSR concurrently developed missiles all of which were based on the V-2 Rocket, and then much longer range Intercontinental Ballistic Missiles (ICBMs). There are now many countries who possess ICBMs and even more with shorter range Intermediate Range Ballistic Missiles (IRBMs). Sub-orbital tourist flights will initially focus on attaining

#131868