| タイトル | Spacecraft for flight in the atmosphere of Venus |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800008874 |
| 著者（英） | Moskalenko, G. M. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 1980-02-01 |
| 言語 | eng |
| 内容記述 | Possible configurations of space vehicles which would be delivered to Venus by rocket system in order to autonomously carry out flights in an automatic (and possibly piloted) mode are considered with respect to mission and flight altitude. Base (high altitude) vehicles, operating at pressure, sendity, and temperature corresponding to those on Earth at sea level, will have little maneuverability, will serve as carriers for equipment, scientific devices, and other cargo, and will study the gas composition of the Venus atmosphere from above. Low altitude vehicles will explore the planet from flight altitude in the vicinity of the planet's surface, as well as land on it. Analogous to deep submergence vehicles such as the bathyscaphe and the bathyplane, they will have a certain amount of maneuverability and will study the atmospheric boundary layer from below. The advantages of aerostats in this environment are discussed. Drawings of the aerostatic base station, the variable-length aerostatic sing vehicle, and the hybrid aerostatic vehicle with attached wings are included. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 80N17134
NASA-TM-75932 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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