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