An “extended” Apollo would be able to travel for several months in space. Garrett concepts of environmental system, cryogenic storage, life-support and attitude control can be adapted to this vehicle.
Space World December 1964, VOL. A-14
Image credit: Marquardt Corporation Image source: Numbers Station
The Marquardt Corporation is conducting studies under contract to North American’s Space and Information Systems Division on advanced rocket reaction control systems for Apollo X. The Extended Apollo Mission is depicted above in conjunction with a space laboratory system, one of several concepts to determine additional applications of the Apollo spacecraft by NASA. Marquardt’s four-engine reaction control system cluster is illustrated above on the surface of the Apollo X service module. Similar systems are being developed by Marquardt for the current Project Apollo lunar mission on both the service and lunar excursion module.
Space World April 1965, VOL. B-4.18
Image credit: Marquardt Corporation Image source: Numbers Station
The MOL – Manned Orbiting Laboratory – is shown, in this artist’s view, being lifted into space by the Titan III C. On top of the cylindrical canister, the crew sit in a modified Gemini capsule.
Orbiting Stations: Stopovers to Space Travel Irwin Stambler G.P. Putnam’s Sons, 1965
Lockheed’s L-2000 SST design, loser in the competition with Boeing for US/SST contract, was result of decade of tunnel testing, incorporating best features of fixed wing double-delta concept proved out in SR-71. Lockheed’s philosophy was simplicity in design for better safety and economy.
How to build an SST! Brilliant Lockheed designer Clarence L. (Kelly) Johnson, who created such successful planes as the U-2, SR-71, F-104 and the Constellation, amused fellow aircrafters with satirical drawing portraying design problems encountered with the SST.
The SST: Here it comes, ready or not by Don Dwiggins Doubleday & Company, Inc., 1968
Image credit: Lockheed Image source: Numbers Station
This drawing from the magazine Air Force and Space Digest shows a proposed NASA “ONE-STAGE-TO-ORBIT” aerospace plane. The craft would be able to take off from a regular airport using turbojet engines, then switch to ramjet propulsion at supersonic speed. To reach orbital speed in space, the aerospace plane would use a third set of engines using rocket propulsion.
In the drawing (above) the combination turbo-ramjet engines are housed in pods, just inside the vertical tailfins (on either side). The huge scoop atop the rear half of the fuselage contains the rocket engines and a novel collection and compression unit for gathering oxygen to burn in the rockets. The other propellant would be liquid oxygen carried in the craft’s tanks.
After it’s orbital mission, the aerospace plane would be able to reenter the atmosphere and land as a conventional aircraft at an airfield. The craft would be about 90 feet long and weigh some 100,000 pounds.
CREDIT LINE (UPI PHOTO) 7-21-62 (ML) UNITED PRESS INTERNATIONAL ROTO SERVICE