FIELD: space engineering. SUBSTANCE: re-entry capsule has separated retro engine 1 and spinning and damping engines 2, separable stabilizing parachute and droppable thermal protection 6. Besides that, capsule has re-entry part which includes payload compartment 10, instrument compartment 9 with devices of control and landing point guidance system, fuel and engine compartment 12 and parachute compartment with landing parachute 24. Secured on fuel and engine compartment 12 is aerodynamic wing 15 and control surfaces 19. Fuel and engine compartment 12 may be made in form of fuel tank with ramjet engine provided with extensible air intake. EFFECT: enhanced reliability. 2 cl, 4 dwg
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| METHOD OF PARACHUTE SYSTEM APPLICATION FOR SALVATION OF CARRIER ROCKET BURNED OUT STAGES OR THEIR PARTS AND DESCENT SPACECRAFT | 2011 |
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RU2495802C2 |
