
Image credit: Boeing Aircraft Company
Image source: Mike Acs

Image credit: NASA
Image source: SDASM Archives

Image credit: NASA
Image source: SDASM Archives




Image credit: Martin
Image source: Ed Dempsey

Image credit: North American Aviation
Image source: Mike Acs

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

Image credit: North American Rockwell
Images: NASA, Mike Acs

Image credit: Convair
Image source: SDASM Archives

A Boeing design for a manned orbital or interplanetary reconnaissance vehicle. The vehicle would be built in orbit around the earth around the Earth, inside a plastic bubble having controlled atmosphere and pressure, permitting technicians to work without space suits. Propelled by a nuclear-powered plasma jet, it could travel to planets within our solar-system , carrying shuttle vehicles to make the actual observations of planet surfaces. Nylon nets, rather than flooring, would divide the vehicle into seven levels.
Eagle Book of Rockets and Space
by John W.R. Taylor and Maurice Allward
Longacre Press, 1961
Image credit: Boeing Aircraft Company
Image source: Numbers Station

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 MSFC
Image source: NASA Images