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- W2316280419 abstract "Cryogenic propulsion is a ver y good option for ELV but is considered as more costly than semi cryogenic (LOX – HC) or bipropellant. On the other hand, a number of new low thrust upper stage concepts have been proposed recently, among them the Low Cost Cryogenic Propulsion (LCCP). LCCP is compared to some other low thrust techniques like Solar Thermal Propulsion and electrically heated hydrogen chemical thrusters. A bipropellant LEO / GTO stage and a high thrust cryogenic upper stage are used for comparison. LCCP provides the best combi nation of mass gain and short transfer time." @default.
- W2316280419 created "2016-06-24" @default.
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- W2316280419 date "2006-07-09" @default.
- W2316280419 modified "2023-10-14" @default.
- W2316280419 title "Low Cost Cryogenic Propulsion as an Option for a New ELV Upper Stage" @default.
- W2316280419 cites W2099804111 @default.
- W2316280419 cites W2312923528 @default.
- W2316280419 doi "https://doi.org/10.2514/6.2006-4905" @default.
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