Athena II

Last updated
  1. 1 2 Wade, Mark. "Athena". Encyclopedia Astronautica. Archived from the original on 29 March 2010. Retrieved 27 March 2010.
  2. "Taurus II" (PDF). Orbital Sciences Corporation. Archived (PDF) from the original on 26 March 2010. Retrieved 27 March 2010.
  3. "Lockheed Martin and ATK Announce 2nd Generation Athena Launch Vehicles". Media - Lockheed Martin. Retrieved 2022-10-10.
  4. Krebs, Gunter. "Athena (LLV / LMLV)". Gunter's Space Page. Archived from the original on 13 February 2010. Retrieved 27 March 2010.
  5. Wade, Mark. "OAM". Encyclopedia Astronautica. Archived from the original on 1 April 2010. Retrieved 27 March 2010.
  6. "Lockheed: Ikonos Fell into Sea". Wired. 29 April 1999. Archived from the original on 4 November 2012. Retrieved 27 March 2010.
  7. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Archived from the original on 7 May 2010. Retrieved 27 March 2010.
Athena II
Athena 2 - Lunar Prospector.jpg
Athena II at LC-46 with Lunar Prospector
FunctionSmall expendable launch system
Manufacturer Lockheed Martin
Alliant Techsystems
Country of originUnited States
Size
Height28.2 metres (93 ft)
Diameter2.36 metres (7 ft 9 in)
Mass120,700 kilograms (266,100 lb)
StagesFour
Capacity
Payload to LEO
Mass2,065 kilograms (4,553 lb)
Comparable Falcon 1
Minotaur IV
Taurus
Launch history
StatusRetired
Launch sites Cape Canaveral LC-46
Vandenberg AFB SLC-6
Total launches3
Success(es)2
Failure(s)1
First flight7 January 1998
Last flight24 September 1999
First stage – Castor 120
Powered by1 solid
Maximum thrust1,900 kilonewtons (430,000 lbf)
Specific impulse 280 sec
Burn time83 seconds
Propellant HTPB