US-PM (US-PU)

Russia


 

US-PM

US-PM (Upravlenniye Sputnik Passivny Modifikirovanny) (also reported as US-PU) was a solar powered improved EORSAT (Electronic Ocean Reconnaisance Satellite). It used an passive ELINT devices to track naval vessels from space by registering their electronic emmissions.

US-PM was a modified version of the US-P and replaced both the US-P and the nuclear US-A satellites.

It shared the same US bus with its precedessors, which provided maneuvering capabilities to the spacecraft.

The US-PM were placed into a 420 km orbits inclined 65 degrees by the Tsiklon-2 booster. Systems aboard the 3300 kg satellite included the Radio-Technical Reconnaissance system and systems for electronic camouflage and self-protection. An engine unit maintained the orbital altitude and made a final deorbit of the satellite at the end of the mission.

Satellite Date LS Launcher Remarks:
Cosmos 2238 [US-PM #1] 31.03.1993 B, LC-90 Tsyklon-2  
Cosmos 2244 [US-PM #2] 28.04.1993 B, LC-90 Tsyklon-2  
Cosmos 2258 [US-PM #3] 07.07.1993 B, LC-90 Tsyklon-2  
Cosmos 2264 [US-PM #4] 17.09.1993 B, LC-90 Tsyklon-2  
Cosmos 2293 [US-PM #5] 02.11.1994 B, LC-90 Tsyklon-2  
Cosmos 2313 [US-PM #6] 08.06.1995 B, LC-90 Tsyklon-2  
Cosmos 2326 [US-PM #7] 20.12.1995 B, LC-90 Tsyklon-2  
Cosmos 2335 [US-PM #8] 11.12.1996 B, LC-90 Tsyklon-2  
Cosmos 2347 [US-PM #9] 09.12.1997 B, LC-90 Tsyklon-2  
Cosmos 2367 [US-PM #10] 26.12.1999 B, LC-90 Tsyklon-2  
Cosmos 2383 [US-PM #11] 21.12.2001 B, LC-90 Tsyklon-2  
Cosmos 2405 (US-PM #12) 28.05.2004 B, LC-90 Tsyklon-2  
Cosmos 2421 (US-PM #13) 25.06.2006 B, LC-90 Tsyklon-2  


Ref.: #7, #14 - update: 3.08.06 Home