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Ramjet
Category of engines.



Subtopics

Co-axial turboramjet Notional LH2-fuelled ramjet engine. Study 1985. Used on Sanger II launch vehicle.

EKR Ramjet Bondaryuk ramjet engine. EKR Stage 2. Study 1953. Study for an experimental winged cruise missile. Not developed but formed basis for Burya and Buran missiles.

RD-012U Bondaryuk ramjet engine. Burya. Out of production. 1.2 m diameter ramjet to be used in Burya cruise missile. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. First flight 1957.

RD-018 Bondaryuk ramjet engine. Buran missile, early version. Out of Production. 1.8 m diameter ramjet engine initially considered for Buran M-42. RD-020 adopted later during development.

RD-020 Bondaryuk ramjet engine. Buran M-42. Development ended 1957. Ramjet for Buran cruise missile. 8,500 km cruise at Mach 3.1 at 18-20 km altitude.

RJ47 Wright ramjet engine. Development ended 1958. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. Used on Navaho G-38 launch vehicle.

XRJ47-W-5 Wright ramjet engine. Out of production. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. Used on Navaho G-26 launch vehicle. First flight 1956.



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