Kistler K-1

Last updated
  1. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 Description of Kistler K-1 on Astronautix Archived 2010-03-24 at the Wayback Machine
  2. 1 2 3 ACCESS TO SPACE FOR EXPLORATION MISSIONS USING REUSABLE LAUNCH VEHICLES
  3. 1 2 Berger, Brian (2007-09-07). "NASA Gives Rocketplane Kistler Termination Notice". Space.com.
  4. "Space Propulsion | Development of U.S. Closed-loop Kerolox Engine Stuck in 2nd Gear". SpaceNews. 2013-07-13. Retrieved 2021-02-22.
  5. 1 2 Mark, Hellman, Barry (2006-01-18). Comparison of Return to Launch Site Options for a Reusable Booster Stage. Georgia Institute of Technology. OCLC   806493663.
  6. "The Kistler K-1 - 1990's Reusable Commercial Rocket - YouTube". www.youtube.com. Archived from the original on 2021-12-22. Retrieved 2021-02-22.
  7. Kistler K-1 Program Status: First Vehicle 75% Complete
  8. "Rocketplane's woes « NewSpace Journal". www.personalspaceflight.info. Retrieved 2021-05-17.
  9. "News & Information Main Page". www.kistler.co. Retrieved 2021-05-17.
  1. 1 2 Includes mass of parachutes and airbags
  2. 1 2 Includes mass of payload bay, heat shield, parachutes, and airbags
Kistler K-1
Kistler K-1.jpg
A render of the K-1 in flight, produced by Rocketplane Kistler
Function Orbital launch vehicle
ManufacturerKistler Aerospace
Country of originUnited States
Size
Height36.9 m (121 ft)
Diameter6.7 m (21.9 ft)
Stages2
Capacity
Payload to Low Earth orbit
Altitude200 km (120 mi)
Orbital inclination45°
Mass4,500 kg (9,900 lb) [1]