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Thruster Assembly and LH2 Tank for the Delta Clipper DC-XA
Thruster Assembly and LH2 Tank for the Delta Clipper DC-XA 
Delta Clipper Team with Liquid Hydrogen Tank
Delta Clipper Team with Liquid Hydrogen Tank 
Delta Clipper Composite Liquid Hydrogen Tank
Delta Clipper Composite Liquid Hydrogen Tank 
Aluminum-Lithium Liquid Oxygen Tank for the Delta Clipper
Aluminum-Lithium Liquid Oxygen Tank for the Delta Clipper 
Delta Clipper Composite Liquid Hydrogen Tank
Delta Clipper Composite Liquid Hydrogen Tank 
Delta Clipper Nearing Completion
Delta Clipper Nearing Completion 
Composite Intertank Assembly for the Delta Clipper
Composite Intertank Assembly for the Delta Clipper 
McDonnel Douglas Employees with Delta Clipper LH2 Tank
McDonnel Douglas Employees with Delta Clipper LH2 Tank 
Fully Assembled DC-X Delta Clipper
Fully Assembled DC-X Delta Clipper 
Delta Clipper Liquid Oxygen Tank
Delta Clipper Liquid Oxygen Tank 
Intertank Assembly for the Delta Clipper
Intertank Assembly for the Delta Clipper 
Delta Clipper Final Assembly
Delta Clipper Final Assembly 
Delta Clipper Avionics Rack
Delta Clipper Avionics Rack 
Delta Clipper Intertank Assembly Detail
Delta Clipper Intertank Assembly Detail 
Delta Clipper Intertank Assembly Detail
Delta Clipper Intertank Assembly Detail 
Delta Clipper Final Assembly
Delta Clipper Final Assembly 
DC-XA Delta Clipper Recovery
DC-XA Delta Clipper Recovery 
Vehicle Management Diagnostics, Telemetry for the Delta Clipper
Vehicle Management Diagnostics, Telemetry for the Delta Clipper 
Interface for the Honeywell Integrated Flight Management Unit Used on the Delta Clipper
Interface for the Honeywell Integrated Flight Management Unit Used on the Delta Clipper 
Delta Clipper Engine Test Fire
Delta Clipper Engine Test Fire 
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Mating the Liquid Hydrogen Tank with the Integrated APU and Liquid Gas Converter on the DC-XA

The Delta Clipper (DC-X) project provided the first hard evidence of the feasibility of achieving a low operational cost, totally reusable rocket system. The DC-X demonstrated low cost, routine ground and flight operations as well as the flight characteristics of a reusable, autonomously controlled vehicle using a liquid oxygen and liquid hydrogen propulsion system. 
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Unique identifier BI229645 
Boeing ID dcx_as21 
Type Image 
Size 2224px × 2811px   17MB 
License type RM 
Keywords
1990s
adults
close-ups
day
factories
factory workers
fuel systems
full body views
ground shots
high-tech / advanced
historic production status
interiors
launch vehicles
lifting
male
manufacturing
one of a kind aircraft
photos
propulsion systems
prototypes
rockets
several/groups
space
spacecraft
three-quarter length views
wires and cables
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