| Cosmos Mariner |
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X-Prize suborbital spaceplane concept of Lone Star Space Access, Houston, Texas. Cosmos Mariner was a concept of Dr. Norman LaFave of Lone Star Space Access, Houston, Texas. The rocketplane would takeoff and land from conventional airfields. Dr. LaFave was a Houston-based physicist who advised NASA on space rendezvous matters. The Cosmos Mariner employed airbreathing jet propulsion for take-off and landing from conventional airports, and rocket propulsion for ascent to 65 km altitude. From there, the vehicle coasted to a target altitude of 120 km. The airframe was designed to interface with two turbofan engines, each with 11,300-kgf static thrust. For rocket propulsion, the Cosmos Mariner was to use three 40,800 kgf thrust, staged-combustion engines. No details of the design ever emerged. Main Engine Thrust: 1,200.300 kN (269,838 lbf). Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. | |||