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McDonnell Douglas DC-X/XA Delta Clipper
Conceptually similar
Fully Assembled DC-X Delta Clipper
Delta Clipper team with DC-X Module at White Sands, NM
DC-X Delta Clipper Launch
Delta Clipper Team with Liquid Hydrogen Tank
DC-X Delta Clipper Hover Test
Delta Clipper Flight Test Team
Delta Clipper Final Assembly
DC-X Delta Clipper Test Module Rollout
Delta Clipper Final Assembly
Delta Clipper Thruster Assembly
DC-XA Delta Clipper Recovery
DC-X Delta Clipper Single-Stage-Rocket-Technology
Delta Clipper Intertank Assembly Detail
Delta Clipper Intertank Assembly Detail
Intertank Assembly for the Delta Clipper
Completed Delta Clipper in Assembly Tower
DC-X Delta Clipper Test Site at White Sands, NM
DC-X Delta Clipper Test Module is Transported to Launch Site
Composite Intertank Assembly for the Delta Clipper
DC-XA Delta Clipper at White Sands, NM
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Delta Clipper Team with Partial DC-X Assembly
The Delta Clipper program was initiated in Huntington Beach in 1991. It was McDonnell Douglas’ version of a single stage reusable launch vehicle. The test product, designated DC-X, was one-third the actual proposed size of the spacecraft. The DC-X was designed to launch and land vertically, and it holds the record for the only single stage reusable launch rocket to have a 26-hour turnaround time between the second and third flights. The teams who worked on this massive project developed software and avionics that allowed the craft to transition smoothly from a vertical takeoff, maneuver in flight in any direction, and land vertically. The Delta Clipper stayed under budget and proved the need for cheaper access to space, incorporated processes that are now industry standard for other aerospace companies.
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Unique identifier
BI629493
Boeing ID
dcx_t02
Type
Image
Size
1098px Ă— 1413px 4MB
License type
RM
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