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Pre-Sputnik Designs
Part of Space Race
Category of launch vehicles.
Subtopics
 | HATV American orbital launch vehicle. Significant Navy program begun in 1946 to develop a single-stage-to-orbit satellite launch vehicle. The Air Force blocked Navy efforts to develop it on a joint basis, while at the same time having no interest in the project itself. Work was abandoned at the end of 1948. |
 | Douglas HATV American orbital launch vehicle. The Douglas HATV design of 1946 was laid out by the Douglas engineer William Ballhaus. He proved that there were no obstacles to a single-stage-to-orbit space launch vehicle, as long as pressurized 'metal balloon' tanks were used instead of using aircraft-structure design approaches. |
 | Martin HATV American orbital launch vehicle. The Martin HATV 1946 design used a single Aerojet engine of unconventional design to achieve single-stage-to-orbit performance. |
 | NAA HATV North American's HATV proposal was an ogival single-stage-to-orbit vehicle, with tanks made from 18-8 stainless steel. In common with other HATV designs, the tanks had to be pressurized to maintain rigidity. |
 | World Circling Space Ship American orbital launch vehicle. Rand study of 1946-1947, in response to the Navy HATV, for a three-stage satellite launcher to be in use by 1952. Development funding was not forthcoming. |
 | EBH LV German orbital launch vehicle. The EBH (Engel - Bödewaldt - Hanischlaunch) vehicle was a 1949 manned design which would had a gross launch mass of 220 metric tons and delivered a payload of 3 metric tons to a 557-kilometre orbit |
| BIS 3 Stage The British Interplanetary Society (BIS) reusable booster concept of 1950 was a 3 stage, rocket, similar to Von Braun concepts of the time. The third stage was a winged vehicle which would use the skip-glide re-entry technique conceived by Saenger. |
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