The potential for converting the space shuttle main engine (SSME) to a dual-fuel, dual-mode engine using LOX/hydrocarbon propellants in mode 1 and LOX/H2 in mode 2 was examined. Various engine system concepts were formulated that included staged combustion and gas generator turbine power cycles, and LOX/RP-1, LOX/CH4, and LOX/C3H8 mode 1 propellants. Both oxidizer and fuel regenerative cooling were considered. All of the SSME major components were examined to determine their adaptability to the candidate dual-fuel engines.
Tripropellant engine study
1978-09-01
Report
Keine Angabe
Englisch
Tripropellant Combustion Investigation
British Library Conference Proceedings | 1996
|Bell annular tripropellant engine concept
AIAA | 1994
|Optimal Control of Gradual Tripropellant Engine for SSTO
AIAA | 2003
|Tripropellant engine tested for SSTO role
Online Contents | 1994