Russian rocket engine. Developed End 40's. Single chamber with turbopump propellant feed.
Status: Developed End 40's.
First Launch: End 40's.
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Associated Countries
See also
Bibliography
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Mikhailov, V S, "Osobennosti Razvitiya Samoletov s Raketnim Dvigatelyami", Issled. Po Ist. I Teorii Razv. Aviat. i Raketo-Kosm. Nauki i Tekhniki, AN SSSR, Moscow 1986.
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