Line drawing of OSCAR 3
Mission typeCommunications
OperatorProject OSCAR
COSPAR ID1965-016F Edit this at Wikidata
SATCAT no.1293
Mission duration16 days
Spacecraft properties
Launch mass15 kilograms (33 lb)
Dimensions7 in × 12 in × 7 in (18 cm × 30 cm × 18 cm)
Start of mission
Launch date9 March 1965, 18:29:47 UTC
RocketThor SLV-2 Agena-D
Launch siteLC-75-1-2
End of mission
Last contactMarch 25, 1965 (1965-03-26)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude884 kilometers (549 mi)
Apogee altitude917 kilometers (570 mi)pe
Inclination70.1 degrees
Period103.1 minutes
Epoch9 March 1965

OSCAR 3 (a.k.a. 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, massing 15 kg (33 lb), was launched piggyback with seven United States Air Force satellites. Though the satellite's active life was limited to sixteen days due to battery failure, OSCAR 3 relayed 176 messages from 98 stations in North America and Europe during its 274 orbit life-time -- the first amateur satellite to relay signals from Earth. As of 2023, it is still in orbit.

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] the similar OSCAR 2, OSCAR 3, and OSCAR 4.[1]


OSCAR 3 was a 15 kg (33 lb) rectangular-prism-shaped satellite, 7 in × 12 in × 17 in (18 cm × 30 cm × 43 cm) in dimension. Unlike its predecessors, which could only transmit a morse code "HI" signal through their beacons, OSCAR 3 was a true communications satellite. Equipped with a translator, when the satellite received signals broadcast to it at 144.1 MHz, its translator converted them to 30 MHz for amplification, and then reconverted them to 145.9 MHz for further amplification and retransmission. A watt of power was available for transmission; if more than one signal were received simultaneously, they shared the power in proportion to their signal strengths when received. OSCAR 3 also carried a beacon like OSCARs 1 and 2, though of lower power.[3]

Four quarter-wave antennas (two for input/output to the translator, one for the beacon, and one for telemetry to the ground) were mounted on the sides of the lightweight magnesium-lithium alloy satellite. The hull was covered with shiny aluminum foil tape to reflect the heat of the Sun, and lack stripes were painted over the shiny aluminum to radiate heat away from OSCAR 3 during the times it orbited in the shadow of the Earth. A large 18-volt battery powered the satellite, though the beacon was designed to continue functioning, supplied by power from solar cells and a rechargeable battery.[3]

Mission and results

Launch of NRL Composite 5 carrying OSCAR 3
Launch of NRL Composite 5 carrying OSCAR 3

OSCAR 3 flew on the NRL Composite 5 mission, which lofted an unprecedented[4] eight satellites on a single Thor Augmented Delta-Agena D rocket (including POPPY 4, an electronic signals intelligence (ELINT) surveillance package, GGSE-2, GGSE-3, Surcal 2B, SECOR 3, SOLRAD 7B, and Dodedcapole 1) on 9 March 1965 from Vandenberg Air Force Base Space Launch Complex 1, Pad 2.[5][6]

Though the satellite's active life was limited to sixteen days due to battery failure,[7] OSCAR 3 relayed 176 messages from 98 stations in North America and Europe during its 274 orbit life-time.[8] The two beacon transmitters continued operating for several months.[9][10] OSCAR 3 was thus the first amateur communications satellite to relay voice contacts in the VHF 2 meter band, the first amateur satellite to operate from solar power and relay signals from Earth, and the first satellite to use beacon transmitters separate from the main communications system.[11]

As of 2023, OSCAR 3 is still in orbit, and its position can be tracked online.[12]


  1. ^ a b 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. ^ a b Robert N. Tellefsen; Harley C. Gabrielson (March 1965). "Oscar III: Ham Radio's New 2-Meter Space Station". Popular Electronics. Vol. 22, no. 3. Ziff-Davis Publishing Co.
  4. ^ "Aeronautics and Astronautics, 1965" (PDF). NASA. Retrieved January 2, 2019.
  5. ^ McDowell, Jonathan. "Launch 1965-016: NRL Composite 5". Jonathon's Space Report. Retrieved March 1, 2020.
  6. ^ McDowell, Jonathan. "Launch Log". Retrieved 2018-12-30.
  7. ^ William R. Corliss (1967). Scientific Satellites. Washington D.C.: Science and Technical Information Division, Office of Technology Utilization, NASA. p. 765. Retrieved 11 May 2020.
  8. ^ H. C. Gabrielson (Dec 1965). "OSCAR 3 Report -- Communications Results" (PDF). QST. pp. 84–89. Retrieved 16 May 2021.
  9. ^ "Oscar 3". NASA National Space Science Data Center. 30 June 1977. Retrieved 15 February 2013.
  10. ^ "OSCAR 3". Gunter's Space Page. 31 December 1999. Retrieved 15 February 2013.
  11. ^ 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.
  12. ^ "OSCAR 3". Retrieved 16 May 2021.