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Tu-121 cruise vehicle
Part of Tu-121 Family
Turbojet powered cruise missile stage. KR-15-300 engine by OKB-300 (now MZ Soyuz), rated for 15 hour endurance.

AKA: Tu-121. Status: Development 1960.. Thrust: 98.00 kN (22,031 lbf). Gross mass: 23,200 kg (51,100 lb). Unfuelled mass: 7,200 kg (15,800 lb). Height: 27.70 m (90.80 ft). Diameter: 1.70 m (5.50 ft). Span: 8.40 m (27.50 ft).

Propellant Formulation: TS or T-1.



Country: Russia. Propellants: Air/Kerosene.

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