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| 1 |
From LH2 tank |
| 2 |
Pump |
| 3 |
Turbine |
| 4 |
Turbopump exhaust |
| 5 |
Nozzle collant pipe (carries entire hydrogen flow) |
| 6 |
Exhaust nozzle |
| 7 |
3% of reactor efflux |
| 8 |
Radiation shield |
| 9 |
Turbine power control valve |
| The thermodynamic nuclear rocket scores over the conventional bi-propellant engine because the LH2 can be heated (without being oxidised) to a much higher temperature, with consequent increase in thrust. |
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