Winston
Lorenzo von Matterhorn
- Joined
- Jan 31, 2009
- Messages
- 9,561
- Reaction score
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The M-1 Rocket Engine Project
https://en.wikipedia.org/wiki/M-1_(rocket_engine)
DEVELOPMENT OF A 1,500,000-LB-THRUST
(NOMINAL VACUUM) LIQUID
HYDROGEN/LIQUID OXYGEN ENGINE
FINAL REPORT
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19680006392.pdf
LO2/ LH2
Thrust (vac.) 1,500,000 lbf (6.67 MN)
Thrust-to-weight ratio 60
Chamber pressure 1,000 psia
Isp (vac.) 428 seconds (4.20 km/s)
Length 7.72 m
Diameter 4.28 m
Dry weight 9068 kg
https://en.wikipedia.org/wiki/M-1_(rocket_engine)
DEVELOPMENT OF A 1,500,000-LB-THRUST
(NOMINAL VACUUM) LIQUID
HYDROGEN/LIQUID OXYGEN ENGINE
FINAL REPORT
https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19680006392.pdf
LO2/ LH2
Thrust (vac.) 1,500,000 lbf (6.67 MN)
Thrust-to-weight ratio 60
Chamber pressure 1,000 psia
Isp (vac.) 428 seconds (4.20 km/s)
Length 7.72 m
Diameter 4.28 m
Dry weight 9068 kg
