Kosmos 242

Kosmos 242
Major contractors Yuzhnoye
Bus DS-P1-I
Mission type ABM Radar target
Launch date 20 September 1968
14:39:59 GMT
Carrier rocket Kosmos-2I 63SM
Launch site Plesetsk Site 133/1
Orbital decay 13 November 1968
COSPAR ID 1968-079A
Mass 325 kilograms (720 lb)
Orbital elements
Regime Low Earth
Inclination 71°
Apoapsis 406 kilometres (252 mi)
Periapsis 272 kilometres (169 mi)
Orbital period 91.3 minutes

Kosmos 242 (Russian: Космос 242 meaning Cosmos 242), also known as DS-P1-I #4 was a satellite which was used as a radar target for anti-ballistic missile tests. It was launched by the Soviet Union in 1968 as part of the Dnepropetrovsk Sputnik programme.[1]

It was launched aboard a Kosmos-2I 63SM rocket,[2] from Site 133/1 at Plesetsk. The launch occurred at 14:39:59 GMT on 20 September 1968.[3]

Kosmos 242 was placed into a low Earth orbit with a perigee of 272 kilometres (169 mi), an apogee of 406 kilometres (252 mi), 71 degrees of inclination, and an orbital period of 91.3 minutes.[1] It decayed from orbit on 13 November 1968.[4]

Kosmos 242 was the fourth of nineteen DS-P1-I satellites to be launched.[1] Of these, all reached orbit successfully except the seventh.[5]

See also

References

  1. ^ a b c Wade, Mark. "DS-P1-I". Encyclopedia Astronautica. http://www.astronautix.com/craft/dsp1i.htm. Retrieved 2009-05-28. 
  2. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. http://planet4589.org/space/log/launchlog.txt. Retrieved 2009-05-28. 
  3. ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. http://www.astronautix.com/lvs/kosmos2.htm. Retrieved 2009-05-28. 
  4. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. http://www.planet4589.org/space/log/satcat.txt. Retrieved 2009-05-28. 
  5. ^ Wade, Mark. "DS". Encyclopedia Astronautica. http://www.astronautix.com/project/ds.htm. Retrieved 2009-05-28.