Engines Using
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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