American space tug. Flown 1968-1982 on Titan 3A and 3C boosters. Transtage mass remaining after insertion of Dynasoar and Abort Stage into orbit. Transtage had its own RCS. Maneuver in earth orbit.
Crew Size: 1. Spacecraft delta v: 450 m/s (1,470 ft/sec).
Gross mass: 3,600 kg (7,900 lb).
More... - Chronology...
Unfuelled mass: 1,950 kg (4,290 lb).
Height: 4.57 m (14.99 ft).
Diameter: 3.05 m (10.00 ft).
Thrust: 71.19 kN (16,004 lbf).
Specific impulse: 311 s.
Dynasoar American manned spaceplane. Cancelled 1963. The X-20A Dyna-Soar (Dynamic Soarer) was a single-pilot manned reusable spaceplane, really the earliest American manned space project to result in development contracts. More...
N2O4/UDMH Nitrogen tetroxide became the storable liquid propellant of choice from the late 1950's. Unsymmetrical Dimethylhydrazine ((CH3)2NNH2) became the storable liquid fuel of choice by the mid-1950's. Development of UDMH in the Soviet Union began in 1949. It is used in virtually all storable liquid rocket engines except for some orbital manoeuvring engines in the United States, where MMH has been preferred due to a slightly higher density and performance. More...
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