OV5-1
From Wikipedia, the free encyclopedia
 OV5-1 | |
| Mission type | Earth science |
|---|---|
| Operator | USAF |
| COSPAR ID | 1967-040E |
| SATCAT no. | S02769 |
| Spacecraft properties | |
| Manufacturer | TRW Inc. |
| Launch mass | 6.3 kg (14 lb) |
| Start of mission | |
| Launch date | 28 Apr 1967 10:01:00 UTC |
| Rocket | Titan IIIC |
| Launch site | Cape Canaveral LC-41 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Highly Elliptical |
| Perigee altitude | 9,484 km (5,893 mi) |
| Apogee altitude | 110,350 km (68,570 mi)[1]: 12 |
| Period | 47.2 hours[2] |
| Epoch | 28 Apr 1967 |
Orbiting Vehicle 5-1 (also known as OV5-1 and ERS 27 [3]), 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.
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
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 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,[4]: 425 versus the analog transmitters used on prior ERS missions.[5] Like prior ERS, the OV5s were spin-stabilized and heat was passively controlled. All of the OV5 series were built by TRW with the exception of OV5-6, built by AFCRL, and OV5-9, built by Northrop Corporation.[4]: 425
With data received OV5-1, the first satellite in the OV5 series, AFCRL hoped to be able to predict the effects of solar activity on the space environment far above the Earth, particularly the strength of hazardous solar protons. The satellite project manager was Major Ronald A. Bena, chief of the Space Forecasting Branch at AFCRL. Dr. G. Kenneth Yates was the project scientist.[2]
Spacecraft design
The OV5 satellites resembled their ERS predecessors. OV5-1 was made of aluminum struts outlining a tetrahedron .3 m (0.98 ft) in width, with 816 solar cells generating 5.5 Watts distributed over the eight triangular faces. The bottom vertex housed the fitting that attached to the launch vehicle; the other vertices were used for mounting experiments. Power was stored in a nickel–cadmium battery. An on-board timer was designed to shut off the satellite after 18 months of operation.[4]: 425
Experiments
The primary experiment on OV5-1 was a proportional counter with a beryllium window for the measurement of X-rays from solar flares. Six directional geiger counters also measured X-rays. The proportional counter also measured background radiation during non-flare periods.[4]: 425 A solar aspect sensor system, determining the angle between the satellite-sun line and the satellite spin axis to within 7.5 degrees, ensured that project scientists could properly interpret satellite data.[6]