SLOMAR at Secret Projects Forum
Image credit: Northrop
Image source: Numbers Station
Tag: cutaway
1969 Mars Mission
Mars Expedition 1969 at Astronautix
Image credit: NASA Lewis
Image source: National Archives
SPACE II
This is a Martin Co. engineering design of a shuttle vehicle to carry five men, or an equivalent amount of equipment, to a rendezvous in orbit with a space station. After delivering it’s load, this vehicle returns to earth by following a glide pattern and slowing in the earth’s atmosphere until landing speed can be attained.
SLOMAR at Secret Projects Forum
Image credit: Martin
Image source: Numbers Station
Mercury
S75-27290
Gary Meyer
Nova Cut-A-Way
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.
- 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
Image source(s):
Orbital Workshop by Neil Jacobe
B&W (As seen in Roundup dated Nov. 24, 1967)
NOV. 67 S-67-51373
MANNED SPACE CENTER, HOUSTON, TEXAS
ORBITAL WORKSHOP — Artist’s concept showing how a Saturn S-IVB stage will appear when converted to the Apollo Applications Orbital Workshop. Launched fully fueled with airlock and docking adaptor attached, the S-IVB’s liquid hydrogen tank becomes a shirtsleeve environment workshop after the fuel has been depleted. At left is an Apollo Command and Service Module launched separately and docked into one of the docking adaptor’s ports. The Apollo Telescope Mount is shown docked into one of the side ports. The ATM will be joined to the cluster in a second phase of the program. Solar cell “wings” to provide power fold outward from the S-IVB after orbit is achieved. McDonnell Douglas Corporation’s Missile and Space Systems Division is making the S-IVB orbital workshop modifications under contract to NASA Marshall Space Flight Center and McDonnell Astronautics Company is developing the airlock under contract to MSC. (MCDONNELL DOUGLAS PHOTOGRAPH)
Look closely and you’ll notice subtle differences between this version of the painting and a colour rendering found in the SDASM Archives I’ve shared before.
If you’re interested in seeing more of Jacobe’s work, his artwork for the Douglas MOL can be found here. The images are small and plastered with watermarks, so it’s a bit of a tease but they are beautiful.
Image credit: NASA
Image source: Numbers Station
Apollo Flight Configuration
The Saturn V configuration is shown in inches and meters as illustrated by the Boeing Company. The Saturn V vehicle consisted of three stages: the S-IC (first) stage powered by five F-1 engines, the S-II (second) stage powered by five J-2 engines, the S-IVB (third) stage powered by one J-2 engine. A top for the first three stages was designed to contain the instrument unit, the guidance system, the Apollo spacecraft, and the escape system. The Apollo spacecraft consisted of the lunar module, the service module, and the command module. The Saturn V was designed perform lunar and planetary missions and it was capable of placing 280,000 pounds into Earth orbit.
Image credit: NASA
Image source: NASA MSFC
numbers station 