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AKA: X-34. Status: Cancelled 2001. Payload: 400 kg (880 lb). Thrust: 386.00 kN (86,776 lbf). Gross mass: 34,000 kg (74,000 lb). Height: 21.95 m (72.01 ft). Diameter: 3.05 m (10.00 ft). Span: 10.37 m (34.02 ft). The original, larger X-34A was powered by an RS-56-OSA Atlas sustainer engine. The 4500 kg third stage was powered by a subscale version of the Fastrac engine.
Payload: 400 kg (880 lb) to a Mach 8, 76 km trajectory. Flyaway Unit Cost 1985$: 3.000 million. Stage Data - X-34
Family: aircraft-launched, orbital launch vehicle. Country: USA. Engines: Fastrac. Stages: X-34A-2, X-34, X-34A-1. Agency: OSC.
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