User:CORONA 0123/sandbox

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CORONA
CORONA (RLV) concept
FunctionPropsed SSTO vehicle
ManufacturerMakeyev Rocket Design Bureau
Country of origin Russia
Size
Height30 metres (98 ft)
Diameter10 metres (33 ft)
Mass30,000 kilograms (66,000 lb)
Stages1
Launch history
StatusDevelopment stopped
First stage
Diameter10 metres (33 ft)
Gross mass30,000 kilograms (66,000 lb)
PropellantLiquid oxygen and liquid hydrogen
Simulated in-flight view of the CORONA
CORONA on launchpad

CORONA was an unmanned prototype of a reusable single-stage-to-orbit launch vehicle developed by Makeyev Rocket Design Bureau from 1992 to 2012. As of the 2013 work curtailed due to lack of funding.

Design[edit]

Evolution of CORONA concept

It is intended for the launch of space vehicles and the spacecraft in the low-Earth circular orbits of 200-500 km. The launch weight of about 300 tons.

See also[edit]

References[edit]

  • New in the development of rocket and space systems: single-stage reusable rocket "CROWN" // Aerospace Technology. Scientific and technical collection. Issue 1 (43) Part 2 / holes. YP Panov, editor EA Osipova. - Miass: SRC "Design Bureau. Academician VP Makeyev ", 1999. - S. 181 - 209. - (XIV). - 400 copies.
  • On the possible ways of development of reusable space transportation systems (MTX) // Aerospace Technology. Scientific and technical collection. Issue 1 (48) Part II / holes. OD Parkhomenko, EA Editor Osipova. - Miass: SRC "Design Bureau. Academician VP Makeyev ", 2002. - S. 120 - 340. - (XIV). - 300 copies.
  • Anton Pervushin. Chapter 15. Heirs "Buran". The "cold" // The battle for the stars. Part II. The cosmic confrontation. - Moscow: OOO "Publishing ACT», 2004. - 831 p.. - 5000 copies -. ISBN 5-17-024200-X.
  • Kosmodem'yanskii AA Konstantin Tsiolkovsky. - 2nd supplemented. - M:. Science, 1987. - 304 p. - 80,000 copies.

External links[edit]