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Conceptually similar
Cutaway Model of the Standard Dyna Soar
Cutaway Model of the Standard Dyna Soar
X-20 Dyna-Soar Model
Cutaway Model of the Advanced Dyna Soar, the X-20X, with Manned Mid-Deck
Dyna-Soar
Dyna-Soar Transtage Separation
Titan III & Dyna-Soar in Flight
Titan III & Dyna-Soar in Ascent
Titan III & Dyna-Soar
X-20 Dyna-Soar on Launch Platform with Titan I
Dyna-Soar Scale Model
Dyna-Soar Scale Model
Dyna-Soar Scale Model
Titan III & Dyna-Soar Jettisons Fuel Tanks
Boeing X-20 Dyna-Soar Astronauts
Dyna-Soar Cockpit
Dyna-Soar Mock-up
Boeing X-20 Dyna-Soar Mock-Up
Boeing X-20 Dyna-Soar Mock-up
Dyna-Soar Configuration Development Diagram
Similar tones
View images with similar tones
Dyna Soar Model with Booster
The X-20 Dyna-Soar, designed to be a 35.5-foot piloted reusable space vehicle, had a sharply swept delta 20.4-foot-span wing and a graphite and zirconia composite nose cap and used three retractable struts for landing. Eleven manned flights were to be launched from Cape Canaveral Fla., starting in November 1964. Dyna-Soar's first orbital flight was tentatively scheduled for early 1965. The X-20 reached the mockup stage. $410 million had been spent on its development, and a cadre of astronauts was training to fly it. However, the U.S. government canceled the program on Dec. 10, 1963, because Dyna-Soar had no viable military mission and was too expensive for a research vehicle.
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Unique identifier
BI222681
Boeing ID
2a130263
Type
Image
Size
4233px × 5362px 64MB
License type
RM
Keywords
1960s
black
blue
Conceptual aircraft, designed, but never produced
engines
full body views
ground shots
high-tech / advanced
historic production status
interiors
launch vehicles
model aircraft
photos
propulsion systems
rocket engines
rockets
space
spacecraft
symmetry
text
white
X-20 Dyna-Soar
Restrictions