330-PSA-279-62 (USAF 167026): Artwork by George Mathis of how the Air Force Titan III Standard Launch Vehicle may look boosting the United States Air Force X-20 (Dyna-Soar) into orbit, August 1962.
Image credit: Boeing Image source: National Museum of U.S. Navy
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.
SOYUZ 16 CONCEPT —- An artist’s concept depicting the Soviet Soyuz 16 spacecraft in Earth orbit. The six-day Soyuz 16 Earth-orbital mission flown December 2-8, 1974, was a Soviet rehearsal for the joint U.S.-USSR Apollo-Soyuz Test Project. The crew of Soyuz 16 was Cosmonauts Anatolly V. Filipophenko, commander; and Hikolay H. Rukavishnikov, engineer. These two me are the Soviet ASTP second (back-up) crew, also. The three major components of the Soyuz spacecraft are the sphere-shaped orbital module, the decent vehicle (in center), and the instrument assembly module. Two solar panels extend out from the IA module. A docking mechanism to test the Soviet ASTP androgenous docking system (seen attached to the orbital module) was flown on the Soyuz 16 flight. This picture was made from a frame of 35mm motion picture film.
PHOTO COURTESY: USSR ACADEMY OF SCIENCES PHOTO CREDIT: NASA or National Aeronautics and Space Administration