Orbiting Vehicle

Orbiting Vehicle or OV, originally designated SATAR (SATellite - Atmospheric Research), comprised several 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.

Not to be confused with orbital vehicle, Orbiter Vehicle, or Orbiter.

"SATAR" redirects here. For other uses, see Satar (disambiguation).

Five separate series of OV satellites were launched. The first. designated OV1, were 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 the cancellation of the Advanced Research Environmental Test Satellite; three OV2 spacecraft flew on Titan IIIC test flights. Space Generall 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 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 ERS project.

Typically, OV satellites carried scientific and/or technological experiments.

History

In the early 1960s, the US Air Force initiated an effort to reduce the expense of space research whereby satellites would be standardized for reliability and cost-efficiency. Space would be utilized on test vehicles and piggyback with other satellites, room permitting. 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.[1]^:417

Summary of launches

Series	Contractor	First launch	Last launch	Built	Launched	Failed to orbit	Remarks
OV1	General Dynamics	1965-01-21	1971-08-07	23	23	4
OV2	Northrop	1965-10-15	1968-09-26	5	3	0
OV3	Aerojet AFRCL	1967-04-22	1967-12-04	6	6	1
OV4	US Air Force Martin Marietta	1966-11-03	1966-11-03	5	3	0
OV5	TRW Systems AFRCL Northrop	1967-04-28	1969-05-23	9	8	1

OV1

A typical OV1 satellite

The OV1 series was originally designed as adaptations 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 were 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 Rangecausing 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.[1]^:417

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[2] 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.

Ultimately, only the first of the SATARs, (OV1-1, called Atmospheric Research Vehicle (ARV) at the time)[3]^:24 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. Typically, 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 a quick experiment proposal-to-launch period of just fifteen months.[1]^:418

OV1 Missions

Name	Mass	COSPAR ID	Launch	Reentry	Remarks
OV1-1	45 kg (99 lb)[3]^:24, 86 kg (190 lb) with Altair booster[4]		21 Jan 1965[3]^:24		Geophysics; first westward launch of a satellite; orbited, but on-board Altair failed to fire.[3]^:24
OV1-2	88 kg	1965 078A	5 Oct 1965		Radiation studies[5]
OV1-3	92 kg (203 lb)[4]		27 May 1965		Biomedical radiation studies; Atlas failed two minutes into flight.[1]^:419
OV1-4	87.5 kg	1966 025A	30 Mar 1966		Thermal control experiments
OV1-5	114 kg	1966 025B	30 Mar 1966		Optical radiation test
OV1-6	202 kg	1966 099C	5 Nov 1966	31 Dec 1966	Inflatable decoy
OV1-7	117 kg		14 Jul 1966		Failed to orbit
OV1-8	3.2 kg	1966 063A	14 Jul 1966	4 Jan 1978	Communications experiment
OV1-9	104 kg	1966 111A	11 Dec 1966		Radiation studies
OV1-10	130 kg	1966 111B	11 Dec 1966	30 Nov 2002	Radiation studies
OV1-11	153 kg		27 July 1967		Failed to orbit
OV1-86	105 kg	1966 072D	27 July 1967	22 Feb 1972	Cosmic ray telescope
OV1-12	140 kg	1966 072D	27 July 1967	22 Jul 1980	Radiation studies; also known as Flare Activated Radio-biological Observatory (Faro)
OV1-13	107 kg	1968 026A	6 Apr 1968		Radiation studies
OV1-14	100 kg	1968 026B	6 Apr 1968		Radiation studies
OV1-15	213 kg	1968 059A	11 July 1968	6 Nov 1968	Air density, solar studies; also known as Solar Perturbation of Atmospheric Density Experiments Satellite (Spades)
OV1-16	272 kg	1968 059B	11 July 1968	19 Aug 1968	Ionospheric drag experiment; also known as Cannonball-1
OV1-17	142 kg	1969 025A	18 Mar 1969	5 Mar 1970	Solar studies
OV1-17A	221 kg	1969 025D	18 Mar 1969	24 Mar 1969	Ionospheric studies; also known as Orbis Cal-2
OV1-18		1969 025B	18 Mar 1969	27 Aug 1972	Ionospheric studies
OV1-19		1969 025C	18 Mar 1969		Radiation studies
OV1-20		1971 061A	7 Aug 1971	28 Aug 1971	Radar calibration, radiation studies
OV1-21		1971 061B	7 Aug 1971		Radar calibration, air density studies

[6]

OV2

OV2-2

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 the Centaur rocket stage, the program's hardware (developed by General Dynamics) was repurposed to fly on the Titan III [1]^:417:422 (initially the A,[7] ultimately the C) booster test launches.[1] The USAF contracted Northrop to produce these satellites, with William C. Armstrong of Northrop Space Laboratories serving as the program manager.[7]

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 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 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 satellite from precessing (wobbling around its spin axis). Passive thermal control kept the satellite from overheating.[1]^:422

OV2 Missions

Name	Mass	COSPAR ID	Launch	Reentry	Remarks
OV2-1	170 kg[8] (59kg experimental payload)	1965 082A	15 Oct 1965	27 Jul 1972	Monitoring biological hazards of near Earth charged particles; failed to separate from LCS-2
OV2-2					Cancelled when the Titan-3C test program was changed; experiments similar to OV2-3
OV2-3	193 kg	1965 108A	21 Dec 1965	17 Aug 1975	Radiation studies; the payload failed to separate from the Transtage and contact was lost after launch.
OV2-4					Cancelled when the Titan-3C test program was changed; designed to observe radiation from trans-lunar orbit
OV2-5	204 kg	1968 081A	26 Sep 1968		Radiation studies: cosmic rays, trapped particle fluxes and changes in fluxes arising from solar and geomagnetic disturbances

[6]

OV3

The Space General-built OV3 series were of octagonal shape measuring 74 cm in diameter and used with Scout launch vehicles.

OV3 Missions

Name	Mass	COSPAR ID	Launch	Reentry	Remarks
OV3-1	68 kg	1966 034A	22 Apr 1966		Radiation studies; Ops-1527
OV3-2	80 kg	1966 097A	28 Oct 1966	29 Sep 1971	Radiation studies
OV3-3	75 kg	1966 070A	4 Aug 1966		Radiation studies
OV3-4	79 kg	1966 052A	10 Jun 1966		Radiation studies; also known as Personnel Hazards Associated with Space Radiation (Phasr) or Ops-1427
OV3-5	94 kg		31 Jan 1967		Ionospheric studies; also known as Atmospheric Composition Satellite (Atcos)-1; failed to orbit
OV3-6	202 kg	1967 120A	4 Dec 1967	9 Mar 1969	Ionospheric studies; also known as Atcos-2

[6]

OV4

The OV4 series was designed to test components of the Manned Orbital Laboratory (MOL) system (later cancelled). The OV4-1 pair of satellites, dubbed "Whispering Gallery", tested the feasibility of using the ionosphere's F layer as a wave guidance for HF and VHF transmissions between satellites out of line of sight of each other.

OV4 Missions

Name	Mass	COSPAR ID	Launch	Reentry	Remarks
OV4-1R	68 kg	1966 099B	3 Nov 1966	5 Jan 1967	"Whispering Gallery" receiver
OV4-1T	109 kg	1966 099D	3-Nov-1966	11-Jan-1967	"Whispering Gallery" transmitter
OV4-2R					"Whispering Gallery" receiver (cancelled)
OV4-2T					"Whispering Gallery" transmitter (cancelled)
OV4-3	9661 kg	1966 099A	3-Nov-1966	9-Jan-1967	Boiler plate model of the Manned Orbiting Laboratory (MOL) to which the reconditioned Gemini-2 (which had been used on a sub-orbital flight on 19 January 1965) was attached; included several experiments; also known as Ops-0855

[6]

OV5

The first six of this series were tetrahedonal spacecraft, also designated Environmental Research Satellites (ERS).

OV5 Missions

Name	Mass	COSPAR ID	Launch	Reentry	Remarks
OV5-1	6 kg	1967 040E	28 Apr 1967		Materials sciences research; also known as ERS-27
OV5-2	10 kg	1968 081B	26 Sep 1968	15 Feb 1971	Radiation studies; also known as ERS-28
OV5-3	8.6 kg	1967 040D	28 Apr 1967		Radiation studies; also known as ERS-20
OV5-4	12 kg	1968 081C	26 Sep 1968		Heat transfer studies; also known as ERS-21
OV5-5	11 kg	1969 046A	23-May-1969		Radiation studies; also known as ERS-29
OV5-6	11 kg	1969 046B	23-May-1969		Solar flare studies; also known as ERS-26
OV5-7					Solar studies; cancelled
OV5-8	9 kg		16 Aug 1968		Materials sciences research – materials friction experiment; failed to orbit
OV5-9	13 kg	1969 046C	23 May 1969		Radiation studies – carried low-energy proton detectors, a dE/dx telescope, a Cerenkov counter, a VLF radiation detector, a solar X-ray monitor and a solar flare electron detector to provide further basic research data on solar radiation and its effects on the magnetosphere

[6]

References

1. 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.
2. Krebs, Gunter. "OV1". Retrieved 24 April 2020.
3. "Aeronautics and Astronautics, 1965" (PDF). NASA. Retrieved 24 April 2020.
4. William R. Corliss (1967). Scientific Satellites. Washington D.C.: Science and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration. pp. 769–776.
5. "OV1- 2". NASA Space Science Data Coordinated Archive. Retrieved November 20, 2019.
6. Heyman, Jos (2005-04-12). "OV". Directory of U.S. Military Rockets and Missiles. Designation Systems. Retrieved February 15, 2020.
7. "OV2-1A Readied for Titan 3 A Test". Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. February 8, 1965. Retrieved February 10, 2020.
8. "OV2-1". NASA Space Science Data Coordinated Archive. Retrieved February 10, 2020.