OV2-3

Summary

OV2-3
OV2SP133.jpg
An OV-2 satellite
Mission typeLife science
OperatorUSAF
COSPAR ID1965-108A
Spacecraft properties
ManufacturerNorthrop
Launch mass194 kg (428 lb)
Start of mission
Launch date22 December 1965, 14:00:01 (1965-12-22UTC14:00:01) UTC
RocketTitan IIIC
Launch siteCape Canaveral LC41[1]
Orbital parameters
Reference systemGeocentric
RegimeHighly elliptical
Eccentricity0.71885
Perigee altitude167 km (104 mi)
Apogee altitude33,662 km (20,917 mi)
Inclination26.300°
Period589.20 minutes[2]
Epoch21 December 1965
← OV2-1
OV2-5 →
 

Orbiting Vehicle 2-3 (COSPAR ID: 1965-108A, also known as OV2-3), the second satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American solar astronomy. geomagnetic and particle science research satellite. Launched 22 December 1965 along with three other satellites, the mission resulted in failure when the spacecraft failed to separate from the upper stage of its Titan IIIC.[2]

Background

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 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 [3]:422 (initially the A,[4] ultimately the C) booster test launches.[3]:422 The USAF contracted Northrop to produce these satellites, with William C. Armstrong of Northrop Space Laboratories serving as the program manager.[4]

The first satellite in the OV2 series, OV2-1, was launched 15 October 1965 with a suite of radiation measuring experiments; it was lost when its booster broke up in orbit.[5] The next satellite in the series, OV2-2, was to carry out optical measurements from an altitude of 400 kilometres (250 mi), but the mission was cancelled when the Titan III test schedule was truncated. Instead, OV2-3, with several solar experiments, was scheduled for the next Titan III launch.[3]:422

Spacecraft design

OV2-3 was built to the configuration standard to all of the OV2 satellites, with a roughly cubical structure of aluminum honeycomb, .61 m (2.0 ft) in height, and .58 m (1.9 ft) wide. Four 2.3 m (7.5 ft) paddle-like solar panels, each with 20,160 solar cells, were mounted at the four upper corners of the main body. The power system, which included NiCd batteries for night-time operations, provided 63 W of power. As with the other craft in the OV2 series, 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.[3]:422 The entire satellite weighed 194 kg (428 lb).[6]

Experiments

The Air Force's Cambridge Research Center in conjunction with Space Systems Division and Aerospace Corporation[4] designed the scientific and engineering experiment package of fifteen instruments designed to measure radiation of solar and geomagnetic origin.[6]

Mission

Titan 3C launch 22 Dec 1965

OV2-3, along with LES-3, LES-4, and OSCAR 4, was launched on the third Titan IIIC test flight[6] on 22 December 1965 at 14:00:01 UT from Cape Canaveral LC41[1] just one second behind schedule. From an initial parking orbit of 194 kilometres (121 mi), the Titan's Transtage boosted into a transfer orbit pending a final burn to circularize its orbit. However, this final burn, scheduled for T+6:03:04 after liftoff,[6] never occurred due to a leaking valve in the booster's attitude control system.[3]:422 LES-3, LES-4, and Oscar 4 were released from the Transtage, albeit much later than intended,[6] but OV2-3 remained attached and did not operate.[3]:422

Legacy and status

The satellite and its transtage are still in orbit as of November 2020.[7]

The OV2 series continued with the radiation and astronomical satellite, OV2-5, which achieved a degree of success.[8]

References

  1. ^ a b McDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved November 26, 2020.
  2. ^ a b "OV2-3". NASA Space Science Data Coordinated Archive. Retrieved 26 November 2020.
  3. ^ a b c d e f g h 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.
  4. ^ a b c "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.
  5. ^ "OV2-1". NASA Space Science Data Coordinated Archive. Retrieved February 10, 2020.
  6. ^ a b c d e "Titan 3 Transtage Malfunctions, Fails to Achieve Circular Orbit". Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. 27 December 1965. p. 27. Retrieved 24 November 2020.
  7. ^ "OV2-3". Retrieved 26 November 2020.
  8. ^ Krebs, Gunter. "OV2". Gunter's Space Page. Retrieved February 12, 2019.

External links

  • Current orbital information for OV2-3. N2YO.com