FIELD: aeronautical engineering. SUBSTANCE: proposed fuel-free system of space vehicle engine plant has fuel tanks with starter-and-cutoff valves, fuel feed manifold of control rocket engines with feed valves and fuel feed main lines connected with starter-and-cutoff valve by cross-feeding pipeline. Fuel-feed system is provided additionally with two cross-feeding main lines with valves uniting tanks and fuel feed manifolds. One additional cross-feeding main line is connected before starter-and-cutoff valve at furl tank outlet, and the other is connected after feed valves before inlet in fuel-feed manifold of control rocket engines. EFFECT: improved performance characteristics of engine plant owing to provision of serviceability of fuel-feed system in case of violation of tightness in fuel main lines and cross-feeding pipelines at long operation in space flight. 1 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| SPACE VEHICLE ENGINE PLANT FUEL-FEED SYSTEM | 1999 | 
 | RU2170840C1 | 
| DEVICE FOR FEEDING PROPELLANT TO SPACECRAFT POWER PLANT | 1999 | 
 | RU2168050C1 | 
| DEVICE TO SUPPLY FUEL TO SPACE CRAFT ENGINE PLANT | 1999 | 
 | RU2160845C1 | 
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| FUEL FEED SYSTEM | 2009 | 
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| SPACECRAFT ENGINE UNIT PROPELLANT TANK PRESSURIZATION SYSTEM | 2000 | 
 | RU2177070C2 | 
| FUEL FEED SYSTEM | 2006 | 
 | RU2339832C2 | 
| FUEL TRANSFER DEVICE | 2003 | 
 | RU2243402C1 | 
| PROPELLANT SUPPLY SYSTEM FOR SPACECRAFT ENGINE PLANT | 2000 | 
 | RU2189485C2 | 
| PRESSURIZATION SYSTEM OF FUEL AND OXIDIZER TANKS OF SPACE FLYING VEHICLE ENGINE PLANT | 1997 | 
 | RU2140003C1 | 
Authors
Dates
2001-07-20—Published
1999-11-05—Filed