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Nuclear 14 Gw
Notional nuclear/LH2 rocket engine. Study 1960. Nuclear second stage Used on Helios B launch vehicle.
Status
: Study 1960.
Thrust
: 3,334.00 kN (749,513 lbf).
Specific impulse
: 830 s.
Burn time
: 355 s.
Family
:
nuclear-powered
.
Country
:
USA
.
Launch Vehicles
:
Helios B
.
Propellants
:
Nuclear/LH2
.
Stages
:
Helios B-2
.
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© 1997-2019 Mark Wade -
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