Engines UsingThis page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |
Engines Using Nuclear/LH2/Methane
| Eng-engineslink |
Thrust(vac)-kgf |
Thrust(vac)-kN |
Isp-sec |
Isp (sea level)-sec |
Designed for |
Status |
RO-31
|
40,000 |
392.00 |
|
|
Upper Stages |
Study 1967 |