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From Wikipedia, the free encyclopedia

Transit 3B
Transit 3B before launch
Mission typeTechnology
OperatorUS Navy
Harvard designation1961 Eta 1
COSPAR ID1961-007A
SATCAT no.87
Spacecraft properties
Launch mass113 kilograms (249 lb)
Start of mission
Launch date22 February 1961 (1961-02-22)
RocketThor DM-21 Ablestar 313/AB-007
Launch siteCape Canaveral LC-17B
End of mission
Decay date30 March 1961
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude167 kilometers (104 mi)
Apogee altitude1,002 kilometers (623 mi)
Inclination28.3 degrees
Period96.4 minutes
Epoch21 February 1961, 22:50:00 UTC[1]

Transit 3B was an American satellite which was launched in 1961 and operated by the United States Navy.[2] It was a replacement for Transit 3A, which was lost in a launch failure the previous year. It carried instruments to demonstrate navigation and timing systems, and study geodesy to support the development of the Transit satellite navigation system.[3]

The launch of Transit 3B was conducted at 03:45 UTC on 22 February 1961, using a Thor DM-21 Ablestar rocket flying from Launch Complex 17B at the Cape Canaveral Air Force Station.[4] The LOFTI-1 satellite was launched aboard the same rocket. The rocket and upper stage used had the serial numbers Thor 313 and Ablestar 007 respectively. The launch resulted in a partial failure, with the spacecraft being placed in a more eccentric orbit than planned, and failing to separate from the upper stage.[3]

Transit 3B was a 113-kilogram (249 lb) spacecraft, which was powered by 6,600 solar cells charging a nickel-cadmium battery. It ended up in a low Earth orbit with a perigee of 167 kilometres (104 mi), an apogee of 1,002 kilometres (623 mi), and 28.3 degrees of inclination. It had an orbital period of 96.4 minutes. Due to the low perigee of its orbit, Transit 3B decayed quickly, and reentered the atmosphere on 30 March 1961, less than 37 days after launch.[5] Despite being in the wrong orbit and operating for less time than had been planned, some useful data was returned from the mission.[3]

The systems demonstrated by Transit 3B included a digital clock to control timing signals, uploading programs into the onboard computer's memory whilst in orbit, data retention and FM encoding, and the use of phase modulation for data transmission without affecting the satellite's Doppler signal. The satellite's computer had a memory capacity of 48 bytes.[6]


  1. ^ "NASA - NSSDCA - Spacecraft - Trajectory Details". Retrieved 2018-05-02.
  2. ^ "Transit 3B". NSSDC Master Catalog. NASA. Retrieved 3 July 2010.
  3. ^ a b c Krebs, Gunter. "Transit-3". Gunter's Space Page. Retrieved 3 July 2010.
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 3 July 2010.
  5. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 3 July 2010.
  6. ^ Wade, Mark. "Transit". Encyclopedia Astronautica. Retrieved 3 July 2010.

This page was last edited on 14 May 2021, at 23:45
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