Discoverer 21

From Wikipedia, the free encyclopedia
Discoverer 21
Mission type Technology
Operator US Air Force/ARPA
Harvard designation 1961 Zeta 1
Spacecraft properties
Bus Agena-B
Manufacturer Lockheed
Launch mass 1,110 kilograms (2,450 lb)
Start of mission
Launch date 18 February 1961, 22:58 (1961-02-18UTC22:58Z) UTC
Rocket Thor DM-21 Agena-B 261
Launch site Vandenberg LC-75-3-5
End of mission
Decay date 20 April 1962 (1962-04-21)
Orbital parameters
Reference system Geocentric
Regime Low Earth
Perigee 243 kilometers (151 mi)
Apogee 1,026 kilometers (638 mi)
Inclination 80.7 degrees
Period 97.4 minutes
The launch of Discoverer 21

Discoverer 21, also known as RM-2, was an American satellite which was launched in 1961. It was a technology demonstration spacecraft, based around an Agena-B.[1]

The launch of Discoverer 21 occurred at 22:58 UTC on 18 February 1961. A Thor DM-21 Agena-B rocket was used, flying from Launch Complex 75-3-5 at the Vandenberg Air Force Base.[2] Upon successfully reaching orbit, it was assigned the Harvard designation 1961 Zeta 1.

Discoverer 21 was operated in a low Earth orbit, with a perigee of 243 kilometres (151 mi), an apogee of 1,026 kilometres (638 mi), 80.7 degrees of inclination, and a period of 97.4 minutes.[3] The satellite had a mass of 1,110 kilograms (2,450 lb),[4] and was used to demonstrate an engine restart,[5] and to test infrared sensors for the Midas programme.[4] It remained in orbit until 20 April 1962,[3] when it decayed and reentered the atmosphere.


References

  1. ↑ Krebs, Gunter. "RM 1, 2 (Discoverer 19, 21)". Gunter's Space Page. Retrieved 30 June 2010. 
  2. ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 30 June 2010. 
  3. ↑ 3.0 3.1 McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 30 June 2010. 
  4. ↑ 4.0 4.1 Wade, Mark. "Midas". Encyclopedia Astronautica. Retrieved 30 June 2010. 
  5. ↑ "Discoverer 21". NSSDC Master Catalog. NASA. Retrieved 30 June 2010. 
Discoverer satellites
← 1960  ·  Orbital launches in 1961  ·  1962 →
Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets.


This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.