Electrothermally augmented hydrazine thruster

Details Electrothermally augmented hydrazine thruster Electrothermally augmented hydrazine thruster

1979-06-18

1981-12-15

Garrett, Robert E.

Power plants

Reaction motor

602031, F02K 0000

Patent

active

043052479

ABSTRACT:
Specific impulse of hydrazine thruster is augmented by electrothermally heating the hot gas in heater passages 36 and 37 as it passes from hydrazine dissociation chamber 14 to thrust nozzle 28. Tubular ceramic electric resistance heater 31 performs primary heating. Specific impulse can be raised from 230 to 300 seconds.

REFERENCES:
patent: 2438865 (1948-03-01), Rehard
patent: 3635824 (1972-01-01), Brandes et al.
patent: 3807657 (1974-04-01), Brill

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