propellant tank, structure, landing gear and a nuclear rocket engine, to be used for landing a payload on Mars and for flying or hopping around. The propellant would be liquid carbon dioxide, easily compressed from the Martian atmosphere; the performance would be, by conventional liquid hydrogen nuclear rocket standards, reasonably awful, but it would be adequate to lurch back into Mars orbit or to do long range hops.
Two main designs seem to have been studied: a conical “ballistic” vehicle that would be a dedicated “hopper,” landing on its tail, and a winded vehicle that would land vertically in a horizontal attitude. This latter design was sent to me in the form of diagrams and five computer renders. The renders – early 1990’s vintage – came as viewgraph transparencies, clearly photographs of a computer monitor. The winged vehicle had simple shock absorbers for landing gear, terminating in dishes rather than wheels meaning that a rolling start or stop was impossible. The available information sadly doesn’t explain how the thing was supposed to land vertically.
The full-rez scans of the viewgraphs have been made available to APR Patrons in the 2016-01 APR Extras Dropbox folder. If you’d like to help out and gain access to this and many other pieces of aerospace history, please check out the APR Patreon.
