Image credit: Douglas
Image source: SDASM Archives
DAC 11835
Category: Launch System
Single-Stage-to-Orbit
- Optional fairing around the two-man Gemini Capsule;
- Gemini adapter section;
- Transition support structure;
- Orbit injection / retro and control propellant tanks (6);
- Toroidal liquid-oxygen tank;
- Annular combustion chamber;
- Truncated plug nozzle and re-entry heat shield;
- Attitude-control system (4);
- Retractable landing legs (4);
- Spherical liquid-hydrogen propellant tank.
Frontiers of Space
Philip Bono & Kenneth Gatland
Macmillan, 1969
Image credit: Douglas
Images: Numbers Station
ROMBUS
Image credit: Douglas
Image source: SDASM Archives
Entry Configuration
Image credit: Douglas
Image source: SDASM Archives
Vehicle Configuration
Image credit: Douglas
Image source: SDASM Archives
DAC 23047
Image credit: Douglas
Image source: SDASM Archive
Clustered Core
Image credit: Douglas
Image source: SDASM Archive
Slide Presentation Scan
Image credit: Douglas
Image source: SDASM Archive
Structural Configuration
Image credit: Douglas
Image source: SDASM Archives
Future Space Taxi
Image credit: Douglas
Image source: Mike Acs
1:60 Scale Model
Image credit: NASA
Image source: SDASM Archives
255-GRC-1964-C-72507
Image credit: NASA
Image source: National Archives
