Minotaur V

Last updated
  1. 1 2 3 "Lunar Atmosphere and Dust Environment Explorer (LADEE) Launch" (PDF). NASA . Retrieved 8 September 2013.
  2. "Lunar Atmosphere and Dust Environment Explorer (LADEE) Mission website". NASA. Archived from the original on 2010-03-29.
  3. 1 2 "Fact Sheet" (PDF). Minotaur V. Orbital Sciences Corporation. Archived from the original (PDF) on 2006-03-11. Retrieved 22 January 2013.
  4. Krebs, Gunter. "Minotaur-3/-4/-5 (OSP-2 Peacekeeper SLV)". Gunter's Space Page. Retrieved 22 January 2013.
  5. Stephen Clark (7 September 2013). "Moon mission hits snag after flawless late-night launch". Spaceflight Now. Retrieved 7 September 2013.
  6. Graham, William (6 September 2013). "Orbital's Minotaur V launches LADEE mission to the Moon". NASAspaceflight.com . Retrieved 8 September 2013.
Minotaur V
Minotaur V carrying LADEE at MARS Pad 0B 2013-09-04.jpg
The first Minotaur V at MARS before the launch of LADEE.
FunctionExpendable launch system
Manufacturer Northrop Grumman (Northrop Grumman Innovation Systems)
Country of originUnited States
Size
Height24.56 m (80.6 ft) [1]
Diameter2.34 m (7 ft 8 in) [1]
Mass89,373 kg (197,034 lb) [1]
Stages5
Capacity
Payload to GTO
Mass532 kg (1,173 lb)