OV1-6

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OV1-6
Titan-3C MOL-Gemini-B-Test 1.jpg
The Titan IIIC on which OV1-6 was launched (mounted just below the Gemini B)
Mission type Earth science
Operator USAF
COSPAR ID 1966-099C OOjs UI icon edit-ltr-progressive.svg
SATCAT no. S02527
Spacecraft properties
Manufacturer General Dynamics
Launch mass202 kg (445 lb)
Start of mission
Launch date2 Nov 1966 13:50:42 (1966-11-02UTC13:50:42) UTC
Rocket Titan IIIC
Launch site Cape Canaveral Space Launch Complex 40
Orbital parameters
Regime Low Earth Orbit
Eccentricity 0.00038
Perigee altitude 290.00 km (180.20 mi)
Apogee altitude 295.00 km (183.30 mi)
Inclination 32.800°
Period 90.40 minutes [1]
Epoch 1966-02-11 13:55:00 UTC
OV1
  OV1-8
OV1-9  
 

Orbiting Vehicle 1-6 (also known as OV1-6 and OV1-6S [2] ) was launched via Titan IIIC rocket into orbit 2 November 1966 along with two other satellites in the United States Air Force's Orbiting Vehicle series on the first and only Manned Orbiting Laboratory test flight. The eighth satellite in the OV1 series to be launched, OV1-6 was designed to release a number of inflatable spheres, which would then be used in classified tracking experiments conducted on the ground. It is uncertain whether or not the satellite successfully released any of its spheres. OV1-6 reentered the Earth's atmosphere on 31 December 1966.

Contents

History

Lt. Col. Clyde Northcott, Jr. , OV1 program manager Lt. Col. Clyde Northcott, Jr. , OV1 program manager.jpg
Lt. Col. Clyde Northcott, Jr. , OV1 program manager

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. [3] :417 Five distinct OV series of standardized satellites were developed under the auspices of these agencies. [3] :425

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 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), 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 the same thrust, and the mass of the SATAR satellites had to be reduced. [3] :417 The OV1 program was managed by Lt. Col. Clyde Northcott, Jr. [4]

Prior to OV1-6, there had been seven satellites in the OV1 series, the first launched January 21, 1965, all on Atlas missiles. [3] :418–422 OV1-6 was programmed for launch out of sequence (after the 14 July 1966 launch of OV1-7 and OV1-8 [2] ) so that it could be carried on the Titan IIIC tasked for the Manned Orbiting Laboratory test flight. [3] :420

Spacecraft design

OV1-6, like the rest of the OV1 satellite series, consisted of a cylindrical experiment housing capped with flattened cones on both ends [5] 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 the sides of the spacecraft. 12 helium-pressurized hydrogen peroxide thrusters provided attitude control. [3] :418 Slightly longer than the standard OV1 satellite, it was 1.7 m (5 ft 7 in) in length. [3] :420

OV1-6 weighed 202 kg (445 lb). [1] It was mounted just behind the Gemini B adapter section on the Titan IIIC rocket. [3] :420 Because the Titan could deliver, by itself, the OV1-6 to its intended orbit, the Altair rocket propulsion unit was removed from the satellite prior to launch. [5]

Experiments

In contrast to prior OV1 satellites, which with the exception of the unique balloon satellite OV1-8, carried onboard instruments for measuring radiation, [3] :418–419 OV1-6 carried several inflatable spheres. These were to be deployed as optical targets for ground tracking experiments conducted by Wright Laboratory at Wright-Patterson Air Force Base. [3] :420 The satellite's purpose was initially classified, [6] with the public story that OV1-6 carried several technical experiments including a zero-gravity propellant gauging system. [7]

Mission

Launched from Cape Canaveral Space Launch Complex 40 on 2 November 1966 at 13:50:42 UTC via Titan IIIC along with a simulated Manned Orbiting Laboratory, a boilerplate Gemini B, and the communications test satellites OV4-1T and OV4-1R, [2] OV1-6 was released after the Titan's Transtage had fired twice to reach the planned 300 km (190 mi) orbit. [3] :424

It is uncertain whether OV1-6 released its target spheres, [3] :420 although at least two additional objects associated with the launch were identified. [2]

Legacy and status

OV1-6 reentered the Earth's atmosphere on 31 December 1966. [8] OV1-6's unused Altair 2 propulsion module was later used, along with OV1-8's unused satellite body, [5] in the construction of OV1-86, launched 27 July 1967. [3] :420 The OV1 program ultimately comprised 22 missions, the last flying on 19 September 1971. [3] :421was eventually used in the construction of OV1-86, launched 27 July 1967. [3] :420 The OV1 program ultimately comprised 22 missions, the last flying on 19 September 1971. [3] :421

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OV1-1 US Air Force satellite

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.

OV1-3 US Air Force satellite

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OV1-2 US Air Force satellite

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.

OV2-3 US Air Force satellite

Orbiting Vehicle 2-3, the second satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American solar astronomy, geomagnetic and particle science research satellite. Launched 22 December 1965 along with three other satellites, the mission resulted in failure when the spacecraft failed to separate from the upper stage of its Titan IIIC.

OV1-4 US Air Force satellite

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.

OV1-5 US Air Force satellite

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.

OV3-1 US Air Force satellite

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.

OV3-4 US Air Force satellite

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.

OV2-5 US Air Force satellite

Orbiting Vehicle 2-5, the third and last satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American particle science and ionosphere research satellite. Launched 26 September 1968 along with three other satellites, OV2-5 became the first scientific satellite to operate at geosynchronous altitude.

OV1-7 US Air Force satellite

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.

OV1-8 US Air Force satellite

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.

OV3-3 US Air Force 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.

OV3-2 US Air Force satellite

Orbiting Vehicle 3-2, 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.

OV1-9 US Air Force satellite

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.

OV1-10 US Air Force satellite

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.

OV3-5 US Air Force satellite

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.

OV1-86 US Air Force satellite

Orbiting Vehicle 1-86 was a satellite launched in the OV1 series of standardized satellites. It was launched with two other satellites in the series, OV1-11 and OV1-12, in the first triple launch of the program, on 27 July 1967. 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 was only a partial success due to the failure of its Vertistat stabilization system. The satellite reentered the Earth's atmosphere on 22 February, 1972.

References

  1. 1 2 "OV1-6". NASA. Retrieved 31 October 2021.
  2. 1 2 3 4 McDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved 31 October 2021.
  3. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 Powell, Joel W.; Richards, G.R. (1987). "The Orbiting Vehicle Series of Satellites". Journal of the British Interplanetary Society. Vol. 40. London: British Interplanetary Society.
  4. "The OV1-Promoter of timely space research". Proceedings of the OAR Research Applications Conference, 14 March 1967. Washington D.C.: Officer of Aerospace Research, United States Air Force. 1967.
  5. 1 2 3 Krebs, Gunter. "OV1" . Retrieved 24 April 2020.
  6. "Space Dizzy Pace". San Francisco Examiner. 13 November 1966. p. 155.
  7. Britannica Book of the Year 1968. Encyclopeaedia Britannica, Inc. 1968. p. 113. OCLC   39721753.
  8. McDowell, Jonathan. "Satellite Catalog". Jonathon's Space Report. Retrieved 31 October 2021.