OSCAR 4

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OSCAR 4
OSCAR 4 interior AMSAT.jpg
OSCAR 4 with exterior panels removed
Mission type Communications
OperatorProject OSCAR / DoD
COSPAR ID 1965-108C
SATCAT no. 01902
Spacecraft properties
Launch mass18.1 kilograms (40 lb)
Start of mission
Launch date21 December 1965 (1965-12-21)
Rocket Titan IIIC 3C-8
Launch site Cape Canaveral LC-41
End of mission
Decay date12 April 1976 (12 April 1976)
Orbital parameters
Reference system Geocentric
Regime Geostationary (planned); Geostationary transfer orbit (actual)
Eccentricity 0.71843
Perigee altitude 162 kilometers (101 mi)
Apogee altitude 33,561 kilometers (20,854 mi)
Inclination 26.80 degrees
Period 587.4 minutes
Epoch 20 December 1965
  OSCAR 3
OSCAR 5  
 

OSCAR IV (a.k.a. OSCAR 4) was the fourth amateur radio satellite launched by Project OSCAR and the first targeted for Geostationary orbit on 12 December 1965. The satellite was launched piggyback with three United States Air Force satellites on a Titan IIIC launch vehicle. Due to a booster failure, OSCAR 4 was placed in an unplanned and largely unusable Geostationary transfer orbit; however, OSCAR 4 did facilitate the first direct satellite communication between the United States and the USSR.

Contents

Project OSCAR

Project OSCAR Inc. was started in 1960 by members of the TRW Radio Club of Redondo Beach, California as well as persons associated with Foothill College to investigate the possibility of putting an amateur satellite in orbit. Project OSCAR was responsible for the construction of the first Amateur Radio Satellites: OSCAR 1, [1] launched from Vandenberg AFB in California on 12 December 1961, which transmitted a “HI” greeting in Morse Code for three weeks, [2] OSCAR 2, and OSCAR 3. [1]

Spacecraft

OSCAR 4 massed 15 kilograms (33 lb) and was a regular tetrahedron with edges 48 centimetres (19 in) long. It had four independent monopole antennae and contained a tracking beacon transmitter and a communications repeater. It was powered by a solar cell array and batteries. [3] The satellite marked the first attempt for a High Earth Orbit (HEO) or GeoStationary Earth Orbit (GEO) amateur radio satellite, later categorized by AMSAT as Phase 3 and Phase 4. Improvements from prior OSCAR satellites included a higher power (3 Watt) 10 kHz wide linear transponder (144 MHz uplink and 432 MHz downlink), due to the higher planned orbit. [4]

Mission

Titan 3C launch 22 Dec 1965 Titan3C launch 22 Dec 1965.jpg
Titan 3C launch 22 Dec 1965

OSCAR 4, along with LES-3, LES-4, and OV2-3, was launched on the third Titan IIIC test flight [5] on 22 December 1965 at 14:00:01 UT from Cape Canaveral LC41 [6] 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, [5] never occurred due to a leaking valve in the booster's attitude control system. [7] :422 OSCAR 4, LES-3 and LES-4, were released from the Transtage, albeit much later than intended, likely by the booster's backup timer; [5] OV2-3 remained attached and did not operate. [7]

Because of its improper orbit, only about 12 two-way communications were established through the OSCAR 4's repeater; however, one on 22 December 1965 was the first direct satellite communication between the United States and the USSR. [3]

The satellite remained in operation for 85 days, until 16 March 1966, and re-entered Earth's atmosphere on 12 April 1976. [8]

Legacy

In 1969, AMSAT-NA was founded by radio amateurs working at NASA's Goddard Space Flight Center and the Baltimore-Washington DC region, to continue the efforts begun by Project OSCAR. Its first project was to coordinate the launch of Australis-OSCAR 5, constructed by students at the University of Melbourne. [4]

See also

Related Research Articles

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Titan IIIC

The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The majority of the launcher's payloads were DoD satellites, for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.

AMSAT-OSCAR 51

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Titan IIIA

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OSCAR 2

OSCAR II is the second amateur radio satellite launched by Project OSCAR into Low Earth orbit. OSCAR II was launched June 2, 1962, by a Thor-DM21 Agena B launcher from Vandenberg Air Force Base, Lompoc, California. The satellite, a rectangular box weighing 10 kg (22 lb), was launched as a secondary payload (ballast) for Corona 43, the fifth launch of a KH-4 satellite.

OSCAR III is the third amateur radio satellite launched by Project OSCAR into Low Earth Orbit. OSCAR 3 was launched March 9, 1965 by a Thor-DM21 Agena D launcher from Vandenberg Air Force Base, Lompoc, California. The satellite, weighing 16.3 kg, was launched piggyback with seven United States Air Force satellites. The satellite employed no attitude control system. OSCAR III linear transponder lasted 18 days. More than 1000 amateurs in 22 countries communicated through the linear transponder. The two beacon transmitters continued operating for several months.

LituanicaSAT-1

LituanicaSAT-1 was one of the first two Lithuanian satellites. It was launched along with the second Cygnus spacecraft and 28 Flock-1 CubeSats aboard an Antares 120 carrier rocket flying from Pad 0B at the Mid-Atlantic Regional Spaceport on Wallops Island to the International Space Station. The launch was scheduled to occur in December 2013, but later was rescheduled to 9 January 2014 and occurred then. The satellite was broadcasting greetings of Lithuanian president, Mrs. Dalia Grybauskaitė. The satellite was deployed from the International Space Station via the NanoRacks CubeSat Deployer on February 28, 2014. All LituanicaSAT-1 subsystems have been turned on, tested and proved to be working properly. The mission is considered a complete success by its team of engineers. The mission ended upon the reentry and disintegration of the satellite on July 28, 2014.

OSCAR 1

OSCAR I is the first amateur radio satellite launched by Project OSCAR into low Earth orbit. OSCAR I was launched December 12, 1961, by a Thor-DM21 Agena B launcher from Vandenberg Air Force Base, Lompoc, California. The satellite, a rectangular box weighing 10 kg., was launched as a secondary payload (ballast) for Corona 9029, also known as Discoverer 36, the eighth and final launch of a KH-3 satellite.

OV2-1 US Air Force satellite

Orbiting Vehicle 2-1, the first satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American life science research satellite. Its purpose was to determine the extent of the threat posed to astronauts by the Van Allen radiation belts. Launched 15 October 1965, the mission resulted in failure when the upper stage of OV2-1's Titan IIIC booster broke up.

LES-1 Former communications satellite

Lincoln Experimental Satellite 1, also known as LES-1, was a communications satellite, the first of nine in the Lincoln Experimental Satellite program. Launched by the United States Air Force (USAF) on February 11, 1965, it pioneered many then-advanced technologies including active use of the military's SHF band to service hundreds of users. LES-1 did not have a successful operational life due to being placed in a suboptimal orbit, but the satellite briefly became significant in its post-operational life when, after more than 40 years of inactivity, it spontaneously resumed transmissions in 2012.

OV1-1 US Air Force satellite

Orbiting Vehicle 1-1, was the first satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-1 was an American Earth science research satellite designed to measure radiation, micrometeoroid density, and magnetic fields in orbit. Launched 21 January 1965, the mission resulted in failure when, after a successful launch of its Atlas booster, OV1-1's onboard Altair motor failed to fire.

OV1-2 US Air Force satellite

Orbiting Vehicle 1-2, launched 5 October 1965, was the third, and first successful, satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. A radiation measuring satellite designed to conduct research for the planned Manned Orbital Laboratory project, OV1-2 was the first American spacecraft to be placed into orbit on a western trajectory. The satellite stopped functioning in April 1967 after a series of technical problems starting two months after launch.

OV2-3 US Air Force satellite

Orbiting Vehicle 2-3, 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.

LES-3 Former communications satellite

Lincoln Experimental Satellite 3, also known as LES-3, was a communications satellite, the third of nine in the Lincoln Experimental Satellite. Launched by the United States Air Force (USAF) on 21 Dec 1965, it was stranded in a Geostationary Transfer Orbit rather than its planned circular high orbit. Despite this, LES-3 returned good data on communications propagation in the UHF band.

LES-4 Former communications satellite

Lincoln Experimental Satellite 4, also known as LES-4, was a communications satellite, the fourth of nine in the Lincoln Experimental Satellite, and the first of the series designed for operations at geosynchronous altitudes. Launched by the United States Air Force (USAF) on 21 December 1965, it demonstrated many then-advanced technologies including active use of the military's SHF band to service hundreds of users.

References

  1. 1 2 Rogerio Atem de Carvalho; Jaime Estela; Martin Langer, eds. (2020). Nanosatellites: Space and Ground Technologies, Operations and Economics. Glasgow: John Wiley & Sons, Ltd. p. 496. ISBN   978-1-119-04203-7. OCLC   1126347525.
  2. "OSCAR 1". NASA Space Science Data Coordinated Archive. Retrieved 26 November 2020.
  3. 1 2 "OSCAR 4". NASA Space Science Data Coordinated Archive. Retrieved 26 November 2020.
  4. 1 2 Baker, Keith; Jansson, Dick (23 May 1994). "Space Satellites from the World's Garage -- The Story of AMSAT". Archived from the original on 5 October 2006. Retrieved 15 February 2013.
  5. 1 2 3 "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.
  6. McDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved November 26, 2020.
  7. 1 2 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. p. 422.
  8. "OSCAR 4". Gunter's Space Page. 31 December 1999. Retrieved 26 November 2020.

PD-icon.svg This article incorporates  public domain material from websites or documents ofthe National Aeronautics and Space Administration .