OV2

 

OV2 5 [USAF]

The OV2 (Orbiting Vehicle 2) series satellites were originally built for project ARENTS (Advanced Research Environmental Test Satellite), which was intended to obtain supporting data for the Vela program. After the cancellation of the ARENTS program, the already built hardware was reused for OV2, a low-cost series of experimental satellites, which were to be launched for free on Titan-3C test flights to very different orbits. OV2 2 would have been launched to a circular 400 km orbit and OV2 4 would have been launched on an earth escape trajectory, but both were cancelled.

Payloads:

  • OV2 1: Subliming solid motor, particle and fields detectors, plasma probes, magnetometers
  • OV2 2: Optical sensors
  • OV2 3: Solar experiments
  • OV2 4: Optical measurements from a highly eccentric trans-lunar orbit
  • OV2 5: 2 scintillation detectors, faraday cup, spherical ion trap, 2 electrostatic analysers, magnetometer, VLF receiver, ORBIS-High beacon, Lyman-alpha scanning UV photometer

OV2 2 and OV2 4 were cancelled, when the Titan-3C test program was changed.

Nation: USA
Type / Application: Experimental
Operator: USAF
Contractors: Northrop Systems Laboratories
Equipment:
Configuration:
Propulsion:
Power: 4 deployable solar arrays, batteries
Lifetime:
Mass: 170 kg (#1); 193 kg (#3); 204 kg (#5)
Orbit: 708 km × 791 km, 32.6° (#1); 167 km × 33662 km, 26.4° (#3); 35084 km × 35774 km, 12.6° (#5);
400 km × 400 km (#2, planned); earth escape (#4, planned)
Satellite Date LS Launch Vehicle Remarks
OV2 1 15.10.1965 CC LC-40 f Titan-3C with LCS 2
OV2 2 cancelled CC Titan-3C with ?
OV2 3 21.12.1965 CC LC-41 p Titan-3C with LES 3, LES 4, Oscar 4
OV2 4 cancelled CC Titan-3C with ?
OV2 5 26.09.1968 CC LC-41 Titan-3C with LES 6, OV5 2, OV5 4