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Titlebook: IXth International Astronautical Congress/IX. Internationaler Astronautischer Kongress/IXe Congrès I; Amsterdam 1958. Band F. Hecht Book 19

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11#
發(fā)表于 2025-3-23 13:22:38 | 只看該作者
IXth International Astronautical Congress/IX. Internationaler Astronautischer Kongress/IXe Congrès I978-3-7091-4745-0
12#
發(fā)表于 2025-3-23 17:13:22 | 只看該作者
13#
發(fā)表于 2025-3-23 21:11:13 | 只看該作者
M. W. Hunter ARS,W. B. Klemperer ARS, AAS,R. J. Gunkel ARS
14#
發(fā)表于 2025-3-24 00:11:54 | 只看該作者
Flight Experiments about Human Reactions to Accelerations which are Followed or Preceded by Weightlf the subject and the efficiency of the physiological recovery mechanisms..The implications for planning of manned space flight are, first, that thrust values and re-entry profiles must take the lower acceleration-tolerance into consideration, and second, that adequate . protection must be designed
15#
發(fā)表于 2025-3-24 03:47:51 | 只看該作者
Magneto-Fluid-Dynamics of Two Interacting Streams, di fluido con proprietà costanti e flusso laminare, le equazioni relative allo strato limite per i seguenti due casi di interazione di due correnti seminfinite elettricamente conduttive in presenza di un campo magnetico: a) campo stazionario rispetto ad un determinato sistema di riferimento; b) cam
16#
發(fā)表于 2025-3-24 07:06:21 | 只看該作者
Impulsive Midcourse Correction of a Lunar Shot,of somewhat idealized Earth-Moon system trajectories. More accurate three-dimensional calculations designed to take the most important perturbations into account were then carried out to verify the applicability of the conclusions to a real case, and to determine its limitations.
17#
發(fā)表于 2025-3-24 11:34:41 | 只看該作者
18#
發(fā)表于 2025-3-24 16:59:04 | 只看該作者
On the Degree of Accuracy, to be Attained by Astro-Scanners as an Aid in Automatic Interplanetary Ce of keeping course on this planet, will be suitable to reach other planets as well. The conclusion drawn is that it is possible (with our present knowledge) to design navigational observation instruments of sufficient accuracy to permit interplanetary navigation with automatic course-computation.
19#
發(fā)表于 2025-3-24 22:39:00 | 只看該作者
Problems of Hypersonic Flight at the Re-Entry of Satellite Vehicles,that is stagnation point flow, similar border lines are established following a discussion by M. C. . and R. F. .. Interesting regions are formed by the intersection of the boundaries for: disappearance of the inviscid flow layer, distinct shock wave, merging of shock wave and flow layer, distinct s
20#
發(fā)表于 2025-3-25 01:33:44 | 只看該作者
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