KARI KSR-3

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search

Template:Short description Script error: No such module "Infobox".Script error: No such module "Check for unknown parameters".

KSR-3 or KSR-III (Korean Sounding Rocket-3)[1] is a South Korean liquid sounding rocket designed by Korea Aerospace Research Institute.[2] It was launched successfully on November 28, 2002 for scientific surveillance purposes.[3] The first test flight of KSR-III was carried out by the KARI rocketry team from Anheung Proving Ground, reaching an altitude of Template:Cvt and flying over Template:Cvt.[4]

Spec

  • Payload: 150 kg
  • Apogee: 42.7 km
  • Range: 79 km
  • Thrust: 13 t
  • Weight: 6.1 t
  • Diameter: 0.42 m
  • Length: 13.5 m
  • Burn time: 53 sec
  • Launch: November 28, 2002[5]

See also

References

  1. ↑ Script error: No such module "citation/CS1".
  2. ↑ Script error: No such module "citation/CS1".
  3. ↑ Script error: No such module "citation/CS1".
  4. ↑ Script error: No such module "citation/CS1".
  5. ↑ Script error: No such module "citation/CS1".

Further reading

Template:South Korean Space Program


Template:Asbox Template:Asbox