CORONA (SSTO)

CORONA

CORONA (RLV) concept
Function Proposed SSTO vehicle
Manufacturer Makeyev Rocket Design Bureau
Country of origin  Russia
Size
Height 30 m (98 ft)
Diameter 10 m (33 ft)
Mass 30,000 kg (66,000 lb)
Stages 1
Launch history
Status development stopped
First stage
Diameter 10 m (33 ft)
Gross mass 30,000 kg (66,000 lb)
Thrust
Fuel Liquid 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

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

References

    External links

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