Athena I

Last updated
  1. Wade, Mark. "Athena". Encyclopedia Astronautica. Archived from the original on 29 March 2010. Retrieved 26 March 2010.
  2. "Lockheed Martin and ATK Announce 2nd Generation Athena Launch Vehicles". Lockheed Martin. 25 March 2010. Archived from the original on 28 March 2010. Retrieved 26 March 2010.
  3. "Taurus II" (PDF). Orbital Sciences Corporation. Archived (PDF) from the original on 26 March 2010. Retrieved 26 March 2010.
  4. Krebs, Gunter. "Athena (LLV / LMLV)". Gunter's Space Page. Archived from the original on 13 February 2010. Retrieved 26 March 2010.
  5. Wade, Mark. "OAM". Encyclopedia Astronautica. Archived from the original on 1 April 2010. Retrieved 26 March 2010.
  6. "Athena I Kodiak Star Launch". NASA. 10 September 2001. Archived from the original on 27 May 2010. Retrieved 26 March 2010.
  7. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Archived from the original on 7 May 2010. Retrieved 26 March 2010.
Athena I
Athena 1 rocket launching from Kodiak Island.jpg
Launch of an Athena I on the Kodiak Star mission.
FunctionSmall expendable launch system
Manufacturer Lockheed Martin
Alliant Techsystems
Country of originUnited States
Size
Height18.9 metres (62 ft)
Diameter2.36 metres (7 ft 9 in)
Mass66,300 kilograms (146,200 lb)
StagesThree
Capacity
Payload to LEO
Mass820 kilograms (1,810 lb)
Derivative work Athena II
Comparable Falcon 1
Minotaur IV
Taurus
Launch history
StatusRetired
Launch sites
Total launches4
Success(es)3
Failure(s)1
First flight15 August 1995
Last flight30 September 2001
First stage – Castor 120
Powered by1 solid
Maximum thrust1,900 kilonewtons (430,000 lbf)
Specific impulse 280 sec
Burn time83 seconds
Propellant HTPB