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X-15A stage
LOx/Ammonia propellant rocket stage. .

AKA: X-15A. Status: Retired 1968. Thrust: 262.45 kN (59,000 lbf). Gross mass: 14,184 kg (31,270 lb). Unfuelled mass: 5,158 kg (11,371 lb). Specific impulse: 276 s. Specific impulse sea level: 239 s. Burn time: 90 s. Height: 15.32 m (50.26 ft). Diameter: 1.42 m (4.65 ft). Span: 6.80 m (22.30 ft).

Cost $ : 100.000 million.

Subtopics
X-15A-2 Tanks LOx/Ammonia rocket stage. Mass 7,026 kg (15,490 lb).
X-15A-2 stage LOx/Ammonia propellant rocket stage. .
Country: USA. Engines: XLR99. Spacecraft: X-15A. Launch Vehicles: X-15. Propellants: Lox/Ammonia.
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