Publikationsdatum:
2019-07-13
Beschreibung:
A consistent engine system data base was generated for defining advantages and disadvantages, system performance and operating limits, engine parametric data, and technology requirements for candidate high pressure LO2/HC engine systems. Optimum LO2/HC engine power cycles were synthetized and representative conceptual engine design generated for a specified advanced surface to orbit transportation system.
Schlagwort(e):
SPACECRAFT PROPULSION AND POWER
Materialart:
NASA-CR-161350
,
MPR-33452M-1
Format:
application/pdf
