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Nuclear 12 Gw
Notional nuclear/LH2 rocket engine. Helios A, Helios C study 1960. Nuclear second stage.
Status
: Study 1960.
Thrust
: 2,892.00 kN (650,147 lbf).
Specific impulse
: 830 s.
Burn time
: 355 s.
Family
:
nuclear-powered
.
Country
:
USA
.
Launch Vehicles
:
Helios A
,
Helios C
.
Propellants
:
Nuclear/LH2
.
Stages
:
Helios A-2
,
Helios C-2
.
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