Space Cruiser
Medium wing load, double delta wing, twin winglet-tails, second stage, spaceplane vehicle. During initial ascent, the cruiser is carried aloft under the lifter on a pylon.

Propulsion:3 Nitrous Oxide/Propane, pressure fed, rocket engines (estimated thrust at 20,000 lb. each); and twin, pylon mounted, JT15D-class turbo-jet engines (estimated thrust at 2.2-4000 lb. each)

Power: Onboard jet engine and/or lifter provided (during captive carry); stored energy, probably battery (during boost, free-fall, retro); ram air turbine (during recovery), onboard jet engine (return to airport)

Crew: Pilot, co-pilot
Passengers: Six (6)
Length: Estimated at 61 ft.
Wing Span: Estimated at 38 ft.
Cabin Size: Estimated at 99 in. (inner diameter), 110 in.(outer diameter), 18 ft. length
Empty Weight: Estimated at 15-20,000 lb.
GTOW: Estimated at 25-30,000 lb.