Mission type | Earth science |
---|---|
Operator | USAF |
COSPAR ID | 1966-097A |
SATCAT no. | S02517 |
Spacecraft properties | |
Manufacturer | Space General |
Launch mass | 81 kg (179 lb) [1] |
Start of mission | |
Launch date | 28 October 1966 11:56:02 UTC |
Rocket | Scout B |
Launch site | Vandenberg Space Launch Complex 5 [2] |
End of mission | |
Decay date | 29 September 1971 |
Orbital parameters | |
Regime | Medium Earth Orbit |
Eccentricity | 0.08697 |
Perigee altitude | 320.00 km (198.84 mi) |
Apogee altitude | 1,597.00 km (992.33 mi) |
Inclination | 82.000° |
Period | 104.20 minutes [3] |
Epoch | 28 October 1966 12:00:00 |
Orbiting Vehicle 3-2 (also known as OV3-2 [3] ), launched 28 October 1966, was the fourth satellite to be launched in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured charged particles in orbit, mapping irregularities in the ionosphere, particularly the auroral zone. OV3-2 reentered the Earth's atmosphere on 29 September 1971.
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, 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. [4] : 417 Five distinct OV series of standardized satellites were developed under the auspices of these agencies. [4] : 425
Unlike the previously initiated OV1 and OV2 series of 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. [4] : 422–423
The first four satellites in 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. [4] : 422–423
Charles H. Reynolds, who worked at AFCRL from 1955, was the technical manager for the OV3 program. [5]
Prior to the launch of OV3-2, three other OV3 satellites had been placed into orbit, all radiation measuring spacecraft launched in 1966. [4] : 423 [2]
Like the rest of the OV3 satellites, OV3-2 was an octagonal prism, .74 m (2 ft 5 in) in length and width, 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, [6] OV3-2 maintained its attitude in orbit with a precession damper. [4] : 422–423 The spacecraft was spin stabilized at eigtht revolutions per minute (rpm) [3] 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. [7] [4] : 423
OV3-2 massed 81 kg (179 lb) [1] Its design life-span was one year. [4] : 423
OV3-2 carried five AFCRL experiments designed primarily to investigate low-energy particles in the Van Allen Belts, [4] : 423 looking for irregularities in the ionosphere, particularly in the auroral zone. [8] In addition to its magnetometer, the spacecraft carried two retarding-potential analyzers (RPA) orthogonally mounted on one 54 in (140 cm) boom [7] and a mass spectrometer, both to detect heavy ions; [4] : 423 a pair [3] of electrostatic analyzers to measure electrons in the 15-80 keV range; [9] and two Langmuir probes on separate 54 in (140 cm) booms to measure electron density in the 0-2 keV range. [7] [4] : 423 The satellite also carried two standing-wave impedance probes on 30 ft (9.1 m) extendable dipoles generating at 2 and 7 Mhz. [7]
Joseph H. Geary was the payload manager for OV3-2. [7]
Launched from Vandenberg Space Launch Complex 5 on 28 October 1966 at 11:56:02 UTC via Scout B rocket into a polar orbit, [3] OV3-2 was the fourth satellite to be launched in the OV3 series. [2] While OV3-2 conducted ionospheric and aurora research in orbit in conjunction with AFCRL KC-135 aircraft flying underneath. [8] The National Research Council of Canada also conducted coordinated, simultaneous ionospheric observations. [10] OV3-2's launch was timed such that it could observe ambient charged particle variations before, during, and after the 12 November 1966 South American solar eclipse. [3]
As a result of the erratic performance of the command system, tape recorded data was not obtained until orbit 58 (four days after launch). [3] In 1967, the tape recorder failed, and an additional command system at Churchill, Manitoba was set up to obtain real-time data. [10] This data had to be manually reduced for interpretation because of a malfunction of OV3-2's onboard clock. Some RPA data was lost due to the failure of the thermal equalization probe. [3] The satellite operated throughout 1967, [9] returning high quality data. [8]
The satellite was tracked from the ground from January 1967 to March 1969, a period of rising solar activity, to determine atmospheric densities at heights of 275 km (171 mi) and 320 km (200 mi). The deduced values were compared to those returned by Explorer 32, also in orbit at the time. Good data were obtained. [3]
OV3-2 reentered the Earth's atmosphere on 29 September 1971. [11]
The OV3 program ultimately comprised 6 missions, five of them successful. The last (OV3-6) flew on 4 December 1967. [2] The OV3 program was terminated following OV3-6 in favor of the cheaper OV1 program. [4] : 423
Orbiting Vehicle or OV, originally designated SATAR, 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.
Orbiting Vehicle 1-1, was the first satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-1 was an American Earth science research satellite designed to measure radiation, micrometeoroid density, and magnetic fields in orbit. Launched 21 January 1965, the mission resulted in failure when, after a successful launch of its Atlas booster, OV1-1's onboard Altair motor failed to fire.
Orbiting Vehicle 1-3, was the second satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-3 was an American life science research satellite designed to measure the effects of orbital radiation on the human body. Launched 28 May 1965, the mission resulted in failure when its Atlas booster exploded two minutes after launch.
Orbiting Vehicle 1-2, launched 5 October 1965, was the third, and first successful, satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. A radiation measuring satellite designed to conduct research for the planned Manned Orbital Laboratory project, OV1-2 was the first American spacecraft to be placed into orbit on a western trajectory. The satellite stopped functioning in April 1967 after a series of technical problems starting two months after launch.
Orbiting Vehicle 1-4, launched 30 Mar 1966, was the fourth, and second successful, satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-4 was a long-term bioscience and materials science satellite, designed to return data relevant to long-term human presence in space. Its launch marked the first time two satellites were placed into orbit side by side with each other.
Orbiting Vehicle 1-5 was launched 30 Mar 1966, and was the fifth satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-5 conducted optical experiments, surveying the Earth in the infrared spectrum to see if water, land, mountains and deserts could be distinguished by their thermal gradients. It was launched concurrently with OV1-4 in the first ever side-by-side satellite orbital deployment.
Orbiting Vehicle 3-1, launched 22 April 1966, was the first satellite in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured radiation above the Earth, returning useful data for over a year. It is still in orbit as of 1 April 2021.
Orbiting Vehicle 3-4, launched 10 June 1966, was the second satellite to be launched in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured radiation above the Earth, helping to determine the hazard posed to human spaceflight at typically traveled altitudes. OV3-4 is still in orbit as of 6 June 2021.
Orbiting Vehicle 1-7, launched 14 July 1966, was the sixth satellite launched in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-7 was a sky science satellite, designed to return data on charged particles in orbit as well as measurements of solar X-rays and nightglow. Co-launched with OV1-8, the satellite was lost when it failed to detach from its launch rocket.
Orbiting Vehicle 1-8, launched 14 July 1966, was the seventh satellite launched in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-8 was designed to test the passive communications utility of an aluminum grid sphere versus a balloon satellite.
Orbiting Vehicle 3-3, launched 4 August 1966, was the third satellite to be launched in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured charged particles in orbit so that their danger to space-based payloads could be assessed. OV3-3 is still in orbit as of 29 July 2021.
Orbiting Vehicle 1-9, launched 11 December 1966 along with OV1-10, was the ninth satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-9 recorded low frequency radio emissions and particle radiation in Earth's exosphere; the satellite also collected data on the impact of long-term radiation on biological samples and tissue equivalents. OV1-9 returned the first proof that Earth has an electric field.
Orbiting Vehicle 1-10, launched 11 December 1966 along with OV1-9, was the tenth satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. Designed to observe atmospheric airglow, X-ray and cosmic radiation, OV1-10 returned significant data on the Sun as well as on geophysical phenomena in Earth's magnetic field. OV1-10 reentered Earth's atmosphere on 30 November 2002.
Orbiting Vehicle 3-5, launched 31 January 1967, was the fifth satellite to be launched in the OV3 series of the United States Air Force's Orbiting Vehicle program.
Orbiting Vehicle 1-86 was a satellite launched 27 July 1967 to measure the temperature radiation properties of different types of terrain. Part of the OV1 series of USAF satellites, using standardized designs and sent to orbit on decommissioned Atlas ICBMs to reduce development and launching costs, OV1-86 was launched with two other satellites in the series, OV1-11 and OV1-12, in the first triple launch of the program. It was the only OV1 satellite to be cobbled together from two of its sister satellites, utilizing the unused body on OV1-8 and the unused propulsion module on OV1-6. OV1-86's was only partially successful due to the failure of its Vertistat gravity-gradient_stabilization system. The satellite reentered the Earth's atmosphere on 22 February 1972.
Orbiting Vehicle 1–12 was a satellite launched 27 July 1967 to measure the radiation hazard posed by solar flares. Part of the OV1 series of USAF satellites, using standardized designs and sent to orbit on decommissioned Atlas ICBMs to reduce development and launching costs, OV1-12 was launched with two other satellites in the series, OV1-11 and OV1-86, in the first triple launch of the program. Only partially successful due to an inability to remain stable in orbit, the satellite reentered the Earth's atmosphere on 22 July 1980.
Orbiting Vehicle 3-6, launched 5 December 1967, was the sixth and last satellite to be launched in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured electron density and neutral density ion composition, as functions of latitude and time. The satellite reentered the Earth's atmosphere on 9 March 1969.
Orbiting Vehicle 5-1, was an X-ray measuring microsatellite launched in support of the United States Air Force's space weather prediction program. Launched on 28 April 1967, it was the first satellite in the OV5 series of the United States Air Force's Orbiting Vehicle program. Data was collected until November 1967, and the satellite turned itself off in June 1967. OV5-1 is still in orbit as of 11 February 2023.
Orbiting Vehicle 1–13 was a satellite launched on 6 April 1968 to measure the level of radiation in orbit at altitudes as high as 8,000 km (5,000 mi). Part of the OV1 series of USAF satellites, using standardized designs and sent to orbit on decommissioned Atlas ICBMs to reduce development and launching costs, OV1-13 was launched side-by-side with OV1-14. The launch marked the first usage of the Atlas F in the OV program. Operating for more than a year and a half, OV1-13 mapped the grosser characteristics of the Van Allen radiation belts and contributed to the understanding of how particles flow and cause increased intensities during solar storms. As of 12 May 2023, OV1-13 is still in orbit.
Orbiting Vehicle 1–16, was launched 11 July 1968 via Atlas F side-by-side with OV1-15. Part of the OV1 series of USAF satellites, OV1-16 was a small, extremely dense sphere, able to withstand air drag much better than a conventional satellite. Along with OV1-15, it was the first satellite to return long-term information on the density and weather patterns of the Earth's upper atmosphere to better predict satellite orbits as well as the splash-down points of reentering satellites and spacecraft. The satellite reentered the Earth's atmosphere on 19 August 1968 after 39 days in orbit.