METHOD OF NEUTRALIZING TOXIC ROCKET FUEL COMPONENTS IN DESCENT STAGE OF ROCKET Russian patent published in 1995 - IPC

Abstract RU 2028468 C1

FIELD: rocket engineering. SUBSTANCE: portion of hydrazine based liquid fuel is supplied to the low pressure pipe line for nitric acid based oxidizer. Gas products of decomposition of oxidizer enter a tank filled with fuel remainder. Reaction products are then discharged to the atmosphere. EFFECT: enhanced quality of neutralizing. 1 dwg

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RU 2 028 468 C1

Authors

Trushljakov V.I.

Shalaj V.V.

Dates

1995-02-09—Published

1991-06-19—Filed