| タイトル | Eliminating LH2 in LOX-collect space launchers - Key to on-demand capability |
| 著者（英） | Maurice, L. Q.; Leingang, J. L.; Carreiro, L. R. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1993-06-01 |
| 言語 | eng |
| 内容記述 | Two air-breathing reusable two-stage space launch vehicle concepts are proposed, in which the first stage employs turboramjet propulsion and the second stage uses rockets, which are expected to provide very rapid response launch of 10,000 lb polar-orbit payloads. In both concepts, liquid oxygen (LOX) for the second stage is collected during first stage ascent, thus eliminating the need for LOX ground servicing facilities. In the first concept, liquid hydrogen in the amount just sufficient to condense and collect second state LOX is the only cryogenic fluid that is loaded on the vehicle at takeoff. The second concept uses the heat sink of conventional jet propulsion fuel and water coolant to drive a lightweight adaptation of the commercial LOX production process, eliminating all cryogenics at takeoff. Both concepts should permit true launch-on-demand capability with aircraftlike ground operations. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 93A49719
AIAA PAPER 93-1835 |
| 権利 | Copyright |
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