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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
Dyna Soar Model with Booster
Boeing X-20 Dyna-Soar Mock-Up
Dyna-Soar Scale Model
Dyna-Soar Scale Model
Dyna-Soar Scale Model
Boeing X-20 Dyna-Soar Mock-up
X-20 Dyna-Soar on Launch Platform with Titan I
Boeing X-20 Dyna-Soar with Wing Skin Removed
Dyna-Soar Cockpit
X-20 Dyna-Soar Structural Glider Design Status Diagram
Dyna-Soar
Boeing X-20 Dyna-Soar Astronauts
Dyna-Soar Transtage Separation
Dyna-Soar Mock-up
Boeing X-20 Dyna-Soar in Orbit
Boeing X-20 Dyna-Soar on Display
Boeing X-20 Dyna-Soar Launch
Similar tones
View images with similar tones
Cutaway Model of the Advanced Dyna Soar, the X-20X, with Manned Mid-Deck
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
BI222677
Boeing ID
2a130260
Type
Image
Size
5305px × 4188px 63MB
License type
RM
Keywords
1960s
blue
brown
Conceptual aircraft, designed, but never produced
copy space
cutaway views
cutouts
engines
full body views
futuristic
ground shots
high-tech / advanced
historic production status
interiors
model aircraft
other livery
passenger cabins
payload systems
photos
POINT OF VIEW
propulsion systems
right front views
rocket engines
space
spacecraft
text
viewed from above
vintage / retro
X-20 Dyna-Soar
Restrictions