OV3

 

OV3 [USAF]

The OV3 (Orbiting Vehicle 3) series were experimental satellites based on an octagonal bus structure. These were the only in the OV series launched on dedicated launchers.

Payloads:

  • OV3 1: Radiation belt particle and fields experiments (reflights of OV2 1 experiments)
  • OV3 2: Low energy radiation belt particles experiments, mass spectrometer, parallel plate retarding-potential analyser, electrostatic analyser, Langmuir probe, triaxial magnetometer
  • OV3 3: Radiation belt particle and fields experiments, Faraday cup, 2 directional telescopes, 3 spectrometers, magnetometer, VLF receiver (reflights of OV2 1 experiments)
  • OV3 4: 6 Tissue equicalent ion chambers, 2 five-channell spectrometers, 2 charged particle spectrometers, magnetometer
  • OV3 5: 2 mass spectrometers (neutal and ionised atmospheric particles), 3 cold cathode ionisation gauges, 2 boom mounted rf impedance probes
  • OV3 6: 2 mass spectrometers (neutal and ionised atmospheric particles), 3 cold cathode ionisation gauges, 2 boom mounted rf impedance probes

OV3 4 was also called PHASR (Personal Hazards Associated with Space Radiation) and OV3 5 and OV3 6 were called ATCOS (Atmospheric Composition Satellite).

Nation: USA
Type / Application: Experimental
Operator: USAF
Contractors: Aerojet (#1 - 4); AFCRL (#5 - 6)
Equipment: see above
Configuration: Aerojet GUS (General Utility Satellite)
Propulsion:
Power: Solar cells, batteries
Lifetime:
Mass:
Orbit:
Satellite Date LS Launch Vehicle Remarks
OV3 1 22.04.1966 Va PALC-D Scout-B
OV3 2 28.10.1966 Va SLC-5 Scout-B
OV3 3 04.08.1966 Va SLC-5 Scout-B
OV3 4 (PHASR) 09.06.1966 WI LA-3 Scout-B
OV3 5 (ATCOS 1) 21.01.1967 Va SLC-5 F Scout-B
OV3 6 (ATCOS 2) 04.12.1967 Va SLC-5 Scout-B