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Orbiting Vehicle or OV , originally designated SATAR (SATellite - Atmospheric Research), comprised five disparate series of standardized American satellites operated by the US Air Force , launched between 1965 and 1971. Forty seven satellites were built, of which forty three were launched and thirty seven reached orbit . With the exception of the OV3 series and OV4-3 , they were launched as secondary payloads, using excess space on other missions. This resulted in extremely low launch costs and short proposal-to-orbit times. Typically, OV satellites carried scientific and/or technological experiments, 184 being successfully orbited through the lifespan of the program.

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53-817: OV2 or variation , may refer to: Orbiting Vehicle 2 (OV2) series of satellites OV2-1 OV2-2 OV2-3 OV2-4 OV2-5 Operational View 2 (OV-2), Operational Node Connectivity British NVC community OV2 , in the UK National Vegetation Classification System .OV2 file format; see List of filename extensions (M–R) See also [ edit ] [REDACTED] Search for "ov2" on Misplaced Pages. All pages with titles beginning with OV2 All pages with titles containing OV2 O2V (disambiguation) OVV (disambiguation) OW (disambiguation) OV (disambiguation) Topics referred to by

106-422: A precession damper. The spacecraft was spin stabilized at 8 revolutions per minute (rpm) A sun sensor, as well as an onboard tri-axial magnetnometer , gave information on the satellite's aspect (facing), its spin rate, and rate of precession . Design life-span was one year. The OV3 program ultimately comprised 6 missions, five of them successful. The last (OV3-6) flew on 4 December 1967. The OV3 program

159-408: A 90° (polar) inclination orbit. In late May 1967, during a period of high solar and magnetic activity, OV1-9 returned the first evidence of Earth's long theorized but never measured electric field. The satellite detected a stream of protons flowing out of the atmosphere into space moving at more than 60,000 km (37,000 mi) per second. OV1-9 also studied the variation of proton fluxes in

212-542: A communications experiment whilst a third, OV4-3, was the primary payload, a boilerplate mockup of the MOL space station. Two further OV4 satellites, duplicates of the first two, were built but not launched. OV5 satellites were launched as secondary payloads on Titan IIIC rockets as part of the Environmental Research Satellite program. The OV program was phased out in the late 1960s, the last of

265-530: A de-orbit module. As announced on 14 October 2014, the United States Department of Defense awarded Sierra Nevada Corporation 's Space Systems (previously known as SpaceDev ) with a contract to develop and build a next-generation science and technology demonstration satellite, known as STPSat-5, for their Space Test Program. The STP-2 (DoD Space Test Program) payload launched aboard a SpaceX Falcon Heavy on 25 June 2019. Included

318-700: A group within the Advanced Systems and Development Directorate , a directorate of the Space and Missile Systems Center of the United States Space Force . STP provides spaceflight via the International Space Station (ISS), piggybacks, secondary payloads and dedicated launch services. STP has actually been in existence for 50 years as of 2019, with several thousand launches it has been responsible for. For example,

371-743: A passive retroreflector. The satellite decayed from orbit on 4 October 2022. (SpaceX had bid a Falcon Heavy in December 2016 for this launch. ) The STP-3 mission was originally scheduled to be launched on a ULA Atlas V 551 launch vehicle in 2020. It was launched on 7 December 2021 at 10:19 UTC . STP-3 includes the STPSat-6 satellite with the Space and Atmospheric Burst Reporting System-3 (SABRS-3) for National Nuclear Security Administration (NNSA), Laser Communications Relay Demonstration (LCRD) payload for NASA, and seven secondary payloads for

424-435: A quick experiment proposal-to-launch period of just fifteen months. The program was managed by Lt. Col. Clyde Northcott, Jr. Data from OV1-4 's Tissue Equivalent Ionization Chamber , compared to a similar instrument orbited on Gemini 4 , determined the radiation dose Gemini astronauts traveling at OV1-4's altitude (~950 km (590 mi)) would receive: 4 rads per day at a 30° inclination orbit or 1.5 rads per day at

477-532: A self-orbiting satellite. Once the Atlas missile and ARS reached apogee, the satellite inside would be deployed and thrust itself into orbit. In addition to the orbital SPP, General Dynamics would create six of these satellites, each to be 3.66 m (12.0 ft) long with a diameter of .762 m (2 ft 6.0 in), able to carry a 136 kg (300 lb) payload into a circular 805 km (500 mi) orbit. Dubbed "Satellite for Aerospace Research" (SATAR),

530-861: A variety of new space technologies. STP and the Air Force Research Laboratory 's (AFRL) Space Vehicles Directorate developed a secondary payload adapter ring for the Evolved Expendable Launch Vehicle (EELV), which can host up to six 180 kg (400 lb) microsatellites . STP also worked closely with NASA and the United States Navy on the Geosynchronous Imaging Fourier Transform Spectrometer / Indian Ocean Meteorology and Oceanography Imager project. In December 2001, STS-108 hosted

583-696: Is a copy of the STPSat-2 satellite, adapted to carry six experiments, including a module designed to host various space situational awareness sensors and a pair of space environment sensors. STPSat 3 launched on 19 November 2013, on the ORS-3 Minotaur 1 launch, along with 28 CubeSats. STPSat-3 carries five payloads, including "Integrated Miniaturized Electrostatic Analyzer Reflight (iMESA-R), Joint Component Research (J-CORE), Strip Sensor Unit (SSU), Small Wind and Temperature Spectrometer (SWATS), and TSI Calibration Transfer Experiment (TCTE)". It also carries

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636-423: Is different from Wikidata All article disambiguation pages All disambiguation pages Orbiting Vehicle The first OV series, designated OV1, was built by General Dynamics and carried on suborbital Atlas missile tests; the satellites subsequently placed themselves into orbit by means of an Altair-2 kick motor . The Northrop -built OV2 satellites were built using parts left over following

689-745: The Centaur rocket stage , the program's hardware (developed by General Dynamics ) was repurposed to fly on the Titan III (initially the A, ultimately the C) booster test launches. The USAF contracted Northrop to produce these satellites, with William C. Armstrong of Northrop Space Laboratories serving as the program manager. The OV2 satellites were all designed on the same plan, roughly cubical structures of aluminum honeycomb, .61 m (2.0 ft) in height, and .58 m (1.9 ft) wide, with four 2.3 m (7.5 ft) paddle-like solar panels mounted at

742-626: The DSTL and the NRL using 6U platforms provided by Blue Canyon Technologies, and they would've flown in formation to study short-timescale dynamics in the ionosphere. The Prometheus 2A and 2B cubesats have been built by In-Space Missions for the UK Ministry of Defence and the NRO and they would've provided a test platform for monitoring radio signals. The STP-CR2301 mission was successfully launched on

795-628: The Deep Space Atomic Clock . The STPSat-4 satellite was launched on 2 November 2019 onboard the Cygnus NG-12 mission and was subsequently deployed to orbit from the ISS on 29 January 2020. The satellite hosted a variety of experimental technologies, including: iMESA-R, a USAF mission to measure plasma densities and energies; MATRS, a modular solar array that partially failed to deploy; NISTEx, an inferometric star tracker; NTE,

848-707: The Kodiak Star mission, in September 2001. On 6 January 2003, STP and the Naval Research Laboratory (NRL) launched the Coriolis satellite, a risk-reduction effort for NPOESS , aboard a Titan II launch vehicle. On 9 March 2007, six satellites were launched into low Earth Orbit (LEO) on a shared Atlas V launch vehicle on the STP-1 mission. The satellites were: The satellites shared

901-474: The U.S. Air Force . STPSat-6 is destined for an orbit slightly above the geostationary orbit. The STP-27VPD mission was launched on LauncherOne 's first mission from Spaceport Cornwall (and last mission overall) on 9 January 2023. The launch resulted in a failure, with the rocket and all its payloads being destroyed in-flight. The mission consisted of two pairs of cubesats from both British and American agencies. The CIRCE 1 and 2 cubesats were developed by

954-457: The 20-50 MHz range. OV4-1R included receiving equipment and telemetry broadcast equipment. Launched into slightly different 300 km (190 mi) orbits, the satellites would test whispering gallery communications over a range of distances; OV4-1T included a small rocket motor to maximize orbital separation (180°) from OV4-1R. Both satellites were cylindrical, .43 m (1 ft 5 in) in diameter, with domed upper ends. Total length

1007-454: The ARSP in 1968. The Space Test Program followed the new trend in satellites, which preferred custom-built one-offs with specific payloads to vehicles built on standardized plans. Space Test Program The Space Test Program ( STP ) is the primary provider of spaceflight for the United States Department of Defense (DoD) space science and technology community. STP is managed by

1060-707: The Air Force Office of Aerospace Research (OAR) created the Aerospace Research Support Program (ARSP) to request satellite research proposals and choose mission experiments. The USAF Space and Missiles Organization created their own analog of the ARSP called the Space Experiments Support Program (SESP), which sponsored a greater proportion of technological experiments than the ARSP. Five distinct OV series of standardized satellites were developed under

1113-626: The Air Force to better predict where and when satellites would decay and reenter. The OV2 series of satellites was originally designed as part of the ARENTS (Advanced Research Environmental Test Satellite) program, intended to obtain supporting data for the Vela satellites, which monitored the Earth for violations of the 1963 Partial Test Ban Treaty . Upon the cancellation of ARENTS due to delays in

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1166-513: The OV2 satellites upon reaching orbit, providing gyroscopic stability. Cold-gas jets maintained this stability, receiving information on the satellite's alignment with respect to the Sun via an onboard solar aspect sensor, and with respect to the local magnetic field via two onboard fluxgate magnetometers. A damper kept the satellites from precessing (wobbling around its spin axis). Passive thermal control kept

1219-466: The OV3 program. The OV3 satellites were octagonal prisms, .74 m (2 ft 5 in) in length and width (for OV3-5 and OV3-6, length was reduced to .53 m (1 ft 9 in)), with experiments mounted on booms. 2560 solar cells provided 30 Watts of power. The satellite was spin-stabilized, but because it was asymmetrical once its booms were extended, OV3-2 maintained its attitude in orbit with

1272-567: The Orbiting Vehicle umbrella. The primary innovation over the earlier ERS series was a command receiver, allowing instructions to be sent from the ground, and a Pulse-code modulation digital telemetry system, versus the analog transmitters used on prior ERS missions. Like prior ERS, the OV5s were spin-stabilized and heat was passively controlled. All of the OV5 series were built by TRW with

1325-689: The Shuttle Ionospheric Modification with Pulsed Localized Exhaust (SIMPLEX) experiment. SIMPLEX observed ionospheric disturbances created by the Space Shuttle engine burns via ground radar sites and supported plume technology, plume signature, and space weather modeling. SIMPLEX flew again on STS-110 in April 2002. STP also worked to obtain a 1-year radio frequency license extension for the Picosat experiment launched on

1378-645: The angle at which protons encountered the satellite also helped refine theoretical models of how the magnetosphere interacts with the flux of charged particles. Unlike the OV1 and OV2 series satellites, which were designed to use empty payload space on rocket test launches, the six OV3 satellites all had dedicated Scout boosters. In this regard, the OV3 series was more akin to its civilian science program counterparts (e.g. Explorer ). OV3 differed from NASA programs in its heavy use of off-the-shelf equipment, which resulted in lower unit cost. The first four satellites in

1431-560: The auspices of these agencies. The OV1 series was an evolution of the 2.7 m "Scientific Passenger Pods" (SPP), which, starting on 2 October 1961, rode piggyback on suborbital Atlas missile tests and conducted scientific experiments during their short time in space. General Dynamics received a $ 2 million contract on 13 September 1963 to build a new version of the SPP (called the Atlas Retained Structure (ARS)) that would carry

1484-600: The cancellation of the Advanced Research Environmental Test Satellite ; three OV2 spacecraft flew on Titan IIIC test flights. Space General built the OV3 satellites, the only series to be launched on dedicated rockets; six were launched on Scout-B rockets between 1966 and 1967. OV4 satellites were launched as part of a test flight for the Manned Orbiting Laboratory (MOL), with two satellites conducting

1537-506: The charged atmosphere of the ionosphere analogous to the whispering gallery transmission of sounds under a physical dome. In this way, the OV4-1 pair would evaluate the ionosphere's F layer as method of facilitating HF and VHF transmissions between satellites not in line of sight of each other. The OV4-1 satellite pair consisted of a transmitting spacecraft and a receiving spacecraft. OV4-1T's transmitter broadcast on three frequencies in

1590-596: The exception of OV5-6, built by AFCRL, and OV5-9, built by Northrop Corporation . The OV program was phased out in the late 1960s, the last of the series (an OV1) flying in 1971. The program orbited 184 experiments at extremely low launch costs and with very short proposal-to-orbit times. OV was succeeded by the Space Test Program , managed by the Space Missile Organization 's Space Experiments Support Program, which had absorbed

1643-479: The first substantial set of data on the density of Earth's atmosphere between the altitudes of 100 km (62 mi) and 200 km (120 mi) and proved that increased solar activity increased the air density at high altitudes, contradicting the prevailing model of the time. Moreover, the satellites determined that the density of the upper atmosphere was 10% lower than predicted by theoretical models. OV1-15/16 data led to improved atmospheric models that allowed

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1696-408: The four upper corners, each with 20,160 solar cells. The power system, which included NiCd batteries for night-time operations, provided 63 W of power. Experiments were generally mounted outside the cube while satellite systems, including tape recorder, command receiver, and PAM/FM/FM telemetry system, were installed inside. Four small solid rocket motors spun, one on each paddle, were designed to spin

1749-631: The initial experiments that led to the modern Global Positioning System (GPS) satellite constellation were STP-launched projects. During August 2001, STP conducted two successful activities using the Space Shuttle and ISS. STS-105 delivered and successfully deployed the Materials International Space Station Experiment (MISSE) externally on the ISS. MISSE was a passive materials exposure experiment,

1802-544: The launcher through use of an Evolved Expendable Launch Vehicle Secondary Payload Adapter ( ESPA ). United Launch Alliance provided a video feed of the launch. The C/NOFS (Communications/Navigation Outage Forecasting System) satellite, which was launched on 16 April 2008, was operated by the Space Test Program. The third Minotaur IV , known as STP-S26 , was successfully launched in November 2010. This

1855-406: The outer Van Allen Belt during that same period, determining that fluxes were ten times greater four days after May's maximum solar activity than they had been before the flare; it took ten days for the fluxes to return to normal levels. The X-ray spectrometer on the co-launched OV1-10 returned the most comprehensive set of solar X-ray observations to date. These data enabled scientists to determine

1908-510: The relative density of neon to magnesium in the solar corona through direct observation rather than using complicated mathematical models. The ratio of neon to magnesium was found to be 1.47 to 1 (+/- .38). OV1-13, launched 6 April 1968, measured increases in energy and intensity of electrons during a geomagnetic storm that took place 10 June 1968. OV1-13 data also clarified how the particle flow caused by solar storms created these high altitude increases. Data returned by OV1s 15 and 16 returned

1961-533: The return of more and more precise data from the satellites. Ultimately, only the first of the SATARs, ( OV1-1 , called Atmospheric Research Vehicle (ARV) at the time) ever flew piggyback on an ABRES mission. The rest were flown on ex-ICBM Atlas D and F boosters specifically purchased by the OAR for the OV1 series (except OV1-6 , which flew on the Manned Orbiting Laboratory test flight on 2 November 1966). Typically,

2014-403: The same term [REDACTED] This disambiguation page lists articles associated with the title OV2 . If an internal link led you here, you may wish to change the link to point directly to the intended article. Retrieved from " https://en.wikipedia.org/w/index.php?title=OV2&oldid=1070482681 " Category : Disambiguation pages Hidden categories: Short description

2067-505: The same thrust, and the mass of the SATAR satellites had to be reduced. The standard OV1 satellite, 1.387 m (4 ft 6.6 in) long and .69 m (2 ft 3 in) in diameter, consisted of a cylindrical experiment housing capped with flattened cones on both ends containing 5000 solar cells producing 22 watts of power. Two .46 m (1 ft 6 in) antennae for transmitting telemetry and receiving commands extended from

2120-510: The satellites from overheating. Three OV2 satellites with different mission objectives were originally planned when the OV2 program began. The OV2 series was ultimately expanded to five satellites, all with different goals. Only OV2-5, a radiation and astronomical satellite, achieved a degree of success. OV2-5 proton energy data collected 2–13 October 1968 in the energy range of 0.060 to 3.3 Mev , showed an eight-fold reduction in particle flux between solar storms and quiet periods. Measuring

2173-417: The satellites were mounted in the nose cone of the launching rocket; OV1-1, OV1-3 and OV1-86 were side mounted. A jettisonable propulsion module with an Altair-2 solid-propellant motor provided the thrust for final orbital insertion. The OV1/Atlas combination was economical for the time, costing just $ 1.25 million per launch ($ 4545 per 1 kg (2.2 lb) of payload). The standardized format also afforded

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2226-522: The series (an OV1) flying in 1971. It was succeeded by the Space Test Program , which focused on tailored satellites with specific payloads rather than standardized ones. The Orbiting Vehicle satellite program arose from a US Air Force initiative, begun in the early 1960s, to reduce the expense of space research. Through this initiative, satellites would be standardized to improve reliability and cost-efficiency, and where possible, they would fly on test vehicles or be piggybacked with other satellites. In 1961,

2279-606: The series of satellites was originally to be launched from the Eastern Test Range on Atlas missions testing experimental Advanced Ballistic Re-Entry System (ABRES) nosecones. However, in 1964, the Air Force transferred ABRES launches to the Western Test Range causing a year's delay for the program. Moreover, because WTR launches would be into polar orbit as opposed to the low-inclination orbits typical of ETR launches, less mass could be lofted into orbit using

2332-463: The series were made the Aerojet subsidiary Space General Corporation under a $ 1.35m contract awarded 2 December 1964, the first satellite due October 1965. The last two satellites were built by Air Force Cambridge Research Laboratory (AFCRL), which also managed the entire series and provided four of the OV3 payloads. Charles H. Reynolds, who worked at AFCRL from 1955, was the technical manager for

2385-490: The sides of the spacecraft. 12 helium-pressurized hydrogen peroxide thrusters provided attitude control. Starting with OV1-7 , the solar cells were flat rather than rounded, and the satellites carried the Vertistat attitude system that used a Sun sensor to determine the spacecraft's orientation to the Sun. OV1-13 and OV1-14 were the first in the OV1 series to use Pulse-code modulation digital telemetry , which afforded

2438-491: Was COSMIC-2 , a cluster of six satellites, with a mass of 277.8 kg (612 lb) each. The primary role of the COSMIC-2 satellite constellation is to provide radio occultation data with an average latency of 45 minutes. The six satellites were placed on an orbit with an inclination of 24° to 28.5° with plans for them to move eventually to six separate orbital planes with 60° separation between them. The payload stack

2491-522: Was .9 m (2 ft 11 in). Silver oxide/zinc batteries provided for a 50-day lifespan. Two sets of OV4 "whispering gallery" satellites were built. OV4-2T and OV4-2R were never flown. OV4-1T and OV4-1R were scheduled for launch on the MOL Heat Shield Qualification flight , with a Titan IIIC rocket. The dummy MOL (a Titan first-stage oxidizer tank) was equipped with a variety of experiments and dubbed OV4-3. OV1-6

2544-463: Was also mounted on the Titan III. The rocket took off from Cape Canaveral Launch Complex 40 on 3 November 1966 at 13:50:42 UTC. The OV5 program was a continuation of the Environmental Research Satellite (ERS) series developed by Space Technology Laboratories , a subdivision of TRW Inc. These were very small satellites launched pick-a-back with primary payloads since 1962—a natural fit under

2597-442: Was demonstrated by deploying two ballast payloads into a 1,200 km (750 mi) orbit. The payload included the STPSat-2 spacecraft. STPSat-2 had 3 three experimental payloads: SPEX (Space Phenomenology Experiment) consisting of two payloads to evaluate sensor compatibility for the space environment, and ODTML (Ocean Data Telemetry MicroSatLink) a two-way data relay from terrestrial (ocean or land) sensors to users. STPSat 3

2650-551: Was integrated using an ESPA ring . Two ESPA Grande rings were used to mount the six COSMIC-2 satellites beneath the upper payload adapter hosting the DSX payload and avionics modules. STP-2 also deployed a number of CubeSats as secondary payloads , including E-TBEx, PSAT, TEPCE, and ELaNa 15 CubeSats. LightSail 2 is carried by the Prox-1 nanosatellite. Other satellites and payloads included Oculus-ASR nanosatellite, GPIM , and

2703-400: Was terminated following OV3-6 in favor of the cheaper OV1 program. The OV4 series was designed to utilize space aboard the Manned Orbiting Laboratory (MOL) test flights. In September 1964, Raytheon was awarded a $ 220,000 contract to build a one-off pair of satellites, designed by the U.S.A.F. Avionics Laboratory . These two satellites would investigate long range radio propagation in

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2756-647: Was the 26th small launch vehicle mission in STP's 40-year history of flying DoD space experiments, STP-S26 launched at 01:45 UTC on 20 November 2010 from the Kodiak Launch Complex . The launch facility contractor was Alaska Aerospace Corporation (AAC). The payloads were released in a 650 km (400 mi) orbit, before the Hydrazine Auxiliary Propulsion System ( HAPS ) upper stage, by Orbital Sciences Corporation ,

2809-521: Was the first external experiment on ISS. In addition, STS-105 retrieved and returned MACE II (Middeck Active Control Experiment II) from the ISS. MACE II was the first internal experiment on ISS and was operated for nearly a year. On 30 September 2001, STP and NASA launched the Kodiak Star mission on an Athena I launch vehicle . This was the first orbital launch out of Kodiak Island , Alaska . In addition to NASA's Starshine III spacecraft, this mission included three small DoD spacecraft which tested

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