Image credit: North American Aviation
Image source: DVIDS
Tag: CSM
Robert Watts
Early Apollo
Gary Meyer
S71-39481
S63-00048
LM Separation
Skylab 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
S-69-60223
Space Station 1970 at Astronautix
Image credit: North American Rockwell
Image source(s):
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
Saturn V Apollo
Skylab
Our World in Space by Isaac Asimov & Robert McCall (1974)
Image credit: NASA
Image source: Numbers Station
