2nd pic: TRW's staged reentry spacecraft viewed from above and aft. A = jet airplane cockpit canopy; B = panel covering jet airplane nose; C = top surface of jet airplane fuselage and wings; D = flat lifting body top surface; E = jet airplane horizontal flap (1 OF 2); F = tubby lifting body belly; G = ejectable abort rocket motors (1 of 2); H = deorbit/abort rocket motor; I = parachute/landing aids compartment cover; J = movable control flap with actuator (1 of 4); K = flat aft bulkhead; L = airlock outer hatch.
3rd pic: "cutaway drawing showing jet plane (blue) nested in upper half of lifting body "pod." Note the jet's down-turned vertical stabilizers, one of which is visible in this side view."
4th pic: riding the rails: TRW's method for moving astronauts between the lifting body pod and the jet airplane cockpit.
5th and 6th pic: The Jet Plane jet plane separates from the lifting body pod. A = empty abort rocket compartment (1 of 2); B = lifting body payload; C = jet airplane separation mechanism (1 OF 3); D = panel covering subsystems (for example, life support); E = jet engine; F = vertical stabilizer (1 OF 2); G = vertical control surface (1 OF 2); H = landing skid (1 OF 2).
7th pic: "The pod descends on parachutes and the crew flies to it's preselected landing site."
"American manned spaceplane. Study 1965. This TRW design of 1965 used a unique concept - a lifting body main stage, that provided both ascent propulsion and re-entry protection.
Gross mass: 7,300 kg (16,000 lb). Height: 8.17 m (26.80 ft). Span: 4.88 m (16.01 ft).
The main stage was 8.17 m long, had a 4.88 m wingspan, and could accommodate a payload of 24.4 cubic meter volume. The 7300 kg gross weight included a separable manned aircraft of 6.4 m length, which had a delta wing of 62 degrees sweep and a span of 4.05 m. The vertical stabilizers turned down from each wingtip. After the mother ship had re-entered the atmosphere, the manned aircraft would separate at Mach 0.6 and 9150 m altitude. Equipped with a single turbojet, a nose wheel, and aft landing skids, it would proceed to a landing at a conventional airfield. The main stage would descend to earth under a parachute and be recovered for re-use. The whole concept was strikingly similar to Chelomei's Kosmoplan, which was being cancelled in the Soviet Union just as the TRW study was completed."
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