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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.

Status: Study 1953. Date: 1953-54. Thrust: 6.13 kN (1,378 lbf). Specific impulse: 1,580 s. Burn time: 800 s.

Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point.

Family: Ramjet. Country: Russia. Launch Vehicles: EKR. Propellants: Air/Kerosene. Stages: EKR Stage 2. Agency: Bondaryuk bureau. Bibliography: 21.
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