Orbiting Vehicle 1–12 (also known as OV1-12[1]) 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 AtlasICBMs 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.
History
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 program, managed by Lt. Col. Clyde Northcott, Jr.[4] 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
Prior to the triple launch of which OV1-12 was a part, there had been ten satellites in the OV1 series launched, the first on January 21, 1965. All were launched on decommissioned Atlas DICBMs, with the exception of OV1-1, the last ABRES test launch, and OV1-6, launched via the Titan IIIC tasked for the Manned Orbiting Laboratory test flight.[3]: 418, 420
Spacecraft design
OV1-12, 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. Continuing the design trend started with OV1-7, the solar cells were flat rather than curved, as had been in the case with the first six OV1 satellites.[3]: 420 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
For stabilization purposes, the satellite was magnetically charged such that it would remain oriented parallel to the Earth's magnetic field, flipping over each time it crossed over one of the Earth's poles.[3]: 420
Experiments
The Air Force Weapons Laboratory equipped OV1-12 with a suite of eleven experiments to study the radiation hazard from solar flares. Called "Flare Activated Radio-biological Observatory" (FARO), the scientific package included a variety of spectrometers and counters to detect electrons and protons as well as a scintillator to measure X-Rays.[2]
Mission
OV1-12 launch (installed in the nose SPP)
OV1-12 was launched from Vandenberg's 576-B-3 launch pad along with OV-11 and OV-86 via Atlas D rocket on 27 July 1967 at 19:00:03 UTC,[1] in the first triple OV1 launch.[3]: 420 Mounted alongside OV-11 in the nose SPP (OV1-86 being installed in a separate, side-mounted SPP), OV1-12 made it into its planned orbit.[6]: 38 The two other experiments included an interferometer and another radiometer to map the Earth in the near-infrared spectrum.[6]: 34 However, the magnetic stabilization system failed to operate as planned, and the satellite tumbled. As a result, only partial data was obtained.[3]: 420
Legacy and status
Despite the spottiness of OV1-12's data set, it was sufficient to produce several published journal articles. These radiation papers, along with ones describing the results of similar devices on OV1-2, energized interest in further study of the radial diffusion of electrons and protons in orbit[7] (i.e. the rate at which they migrate to different heights above the Earth).[8]
OV1-12 reentered the Earth's atmosphere on 22 July 1980.[2] The OV1 program ultimately comprised 22 missions, the last flying on 19 September 1971.[3]: 421
References
^ abcMcDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved 22 July 2022.
^ abcdefghijPowell, Joel W.; Richards, G.R. (1987). "The Orbiting Vehicle Series of Satellites". Journal of the British Interplanetary Society. Vol. 40. London: British Interplanetary Society.
^"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.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).
