Design a site like this with WordPress.com
Get started

Phil Santos

SASSTO at Astronautix

Image credit: Douglas

Image source: SDASM Archives

Martian Habitat / Gentlemen’s Club

Boeing Mars Glider at Astronautix

Image credit: Boeing

Image source: SDASM Commons

Removing The Reactor

Boeing Mars Glider at Astronautix

Image credit: Boeing

Image source: SDASM Commons

Exploration & Utility Vehicle

Boeing Mars Glider at Astronautix

Image credit: Boeing

Image source: SDASM Commons

Mars Launch Vehicle

Boeing Mars Glider at Astronautix

Image credit: Boeing

Image source: SDASM Commons

All-Purpose Space Vehicle

  1. All-purpose space vehicle proposed by Douglas Missile & Space Systems Division engineer Phil Bono, is pictured in artist’s concept during refueling in earth orbit prior to flight to the moon.
  2. Refueling tankers, on either side will return to earth. Vehicle carries up to eight “strap-on” liquid hydrogen tanks, which can be ejected after they are emptied or retained for use on moon. Retro engines are fire as spacecraft nears lunar surface to allow a direct landing without an orbital maneuver. All-purpose space vehicle proposed by Douglas Missile & Space Systems Division engineer Phil Bono, is pictured in artist’s concept during refueling in earth orbit prior to flight to the moon.
  3. Empty strap-on tanks are lowered to lunar surface before each return flight.
  4. These liquid hydrogen tanks could be used as shelter for pioneering lunar colony.

Space World

December 1964, VOL. A-14

Project Selena at Astronautix

Image credit: Douglas

Image source: Numbers Station

Ithacus B&W Plates

Ithacus at Astronautix

Image credit: Douglas

Image source(s):

Mike Acs

SDASM Archives

SASSTO

SASSTO (Saturn Application Single-Stage-to-Orbit) combined launch vehicle and spacecraft. Only 62.3 ft (19m.) tall, a single plug-nozzle engine would serve both as launch vehicle and for soft-landing back on Earth after an orbital mission. The craft – seen here with a Gemini two-man capsule – would be recovered intact and could be used repeatedly. It would be a particularly appropriate for ferry missions into Earth-orbit including the emergency rescue of astronauts.

  1. Optional fairing around the two-man Gemini Capsule;
  2. Gemini adapter section;
  3. Transition support structure;
  4. Orbit injection / retro and control propellant tanks (6);
  5. Toroidal liquid-oxygen tank;
  6. Annular combustion chamber;
  7. Truncated plug nozzle and re-entry heat shield;
  8. Attitude-control system (4);
  9. Retractable landing legs (4);
  10. Spherical liquid-hydrogen propellant tank.

Frontiers of Space
Philip Bono & Kenneth Gatland
Macmillan, 1969

SASSTO at Astronautix

Image credit: Douglas

Image source(s):

SDASM Archives

Numbers Station

Ithacus Explained

  1. Ithacus troop transport launched from a nuclear carrier;
  2. Troops disembark from Ithacus rocket at their destination halfway across the world;
  3. After transfer from the interior, empty vehicle is taken by barge to a convenient coastal spaceport for reconditioning and relaunch.

Ithacus at Astronautix

Image credit: Douglas

Image source: SDASM Archives