LIQUID-PROPELLANT ROCKET ENGINE TEST METHOD Russian patent published in 1995 - IPC

Abstract RU 2050459 C1

FIELD: test technique. SUBSTANCE: similar engines are placed in common altitude chamber; natural vacuum conditions are created about them and at nozzle edges; fuel is supplied from common power supply and engines are fired simultaneously. EFFECT: facilitated procedure. 1 dwg

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RU 2 050 459 C1

Authors

Andreev P.P.

Baklykov Ju.D.

Gudkov M.M.

Erofeev B.S.

Fabrin Ju.N.

Dates

1995-12-20Published

1992-04-24Filed