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標(biāo)題: Titlebook: Apollo; The Definitive Sourc Richard W. Orloff,David M. Harland Book 2006 Springer-Verlag New York 2006 Apollo.Orloff.Reference.Statistical [打印本頁(yè)]

作者: 不足木    時(shí)間: 2025-3-21 17:41
書目名稱Apollo影響因子(影響力)




書目名稱Apollo影響因子(影響力)學(xué)科排名




書目名稱Apollo網(wǎng)絡(luò)公開度




書目名稱Apollo網(wǎng)絡(luò)公開度學(xué)科排名




書目名稱Apollo被引頻次




書目名稱Apollo被引頻次學(xué)科排名




書目名稱Apollo年度引用




書目名稱Apollo年度引用學(xué)科排名




書目名稱Apollo讀者反饋




書目名稱Apollo讀者反饋學(xué)科排名





作者: 不遵守    時(shí)間: 2025-3-21 23:40

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作者: Employee    時(shí)間: 2025-3-22 13:44
,Apollo 9: The third manned mission: testing the LM in Earth orbit 3–13 March 1969,
作者: Heterodoxy    時(shí)間: 2025-3-22 17:52
,Apollo 10: The fourth manned mission: testing the LM in lunar orbit 18–26 May 1969,
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,Apollo 11: The fifth manned mission: the first lunar landing 16–24 July 1969,
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,Apollo 15: The ninth manned mission: the fourth lunar landing 26 July–7 August 1971,
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,Apollo 16: The tenth manned mission: the fifth lunar landing 16–27 April 1972,
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作者: Ceramic    時(shí)間: 2025-3-23 22:47
,Saturn I: Development program 1961–1965,s had required to be shut down, and in that case the vehicle had compensated for its loss. But despite its rapid development and flight record the Saturn I had been overtaken by events and was declared obsolete.
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作者: 命令變成大炮    時(shí)間: 2025-3-24 06:39
AS-203: The second flight of the Saturn IB: evaluating the S-IVB 5 July 1966,g coasting flight provided sufficient ullage to maintain the hydrogen settled in its tank, as would be required on a Saturn V dispatching a lunar mission. The simulated restart verified the chilldown and recirculation systems of the J-2 engine. AS-203 was therefore a successful test of the S-IVB stage.
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Apollo 5: Unmanned test of the LM 22 January 1968,Despite the switch to an alternative plan following the premature shutdown of the first DPS firing, the overall performance of the LM met all of the requirements for manned orbital flight and the planned second test flight was cancelled.
作者: 富足女人    時(shí)間: 2025-3-25 09:57

作者: 盤旋    時(shí)間: 2025-3-25 15:25
Richard W. Orloff,David M. HarlandProvides a comprehensive collection of tables listing facts and figures for each mission.Gives a comprehensive statistical reference of the program.Single-volume sourcebook on the program.This complet
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作者: profligate    時(shí)間: 2025-3-25 22:37
Elementary Mechanics Using Matlabs had required to be shut down, and in that case the vehicle had compensated for its loss. But despite its rapid development and flight record the Saturn I had been overtaken by events and was declared obsolete.
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作者: 皺痕    時(shí)間: 2025-3-26 10:47
Elementary Mechanics Using Matlabs had required to be shut down, and in that case the vehicle had compensated for its loss. But despite its rapid development and flight record the Saturn I had been overtaken by events and was declared obsolete.
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作者: Charlatan    時(shí)間: 2025-3-26 17:26
https://doi.org/10.1007/978-3-319-19596-4g coasting flight provided sufficient ullage to maintain the hydrogen settled in its tank, as would be required on a Saturn V dispatching a lunar mission. The simulated restart verified the chilldown and recirculation systems of the J-2 engine. AS-203 was therefore a successful test of the S-IVB sta
作者: 軟膏    時(shí)間: 2025-3-26 22:13
Sums of an Even Number of Squaresthe Block II heat shield for entry at lunar return conditions. These objectives were satisfactorily accomplished..The spacecraft subsystems operated satisfactorily in all respects. Performance of the guidance and control subsystems was equal to or better than predictions. All sequencing and computat
作者: Brittle    時(shí)間: 2025-3-27 01:20
Apollo 4: The first test of the Saturn V 9 November 1967,ional operations performed by the guidance computer were correct. The environmental control subsystem maintained the cabin pressure and temperature within required limits. The thermal protection subsystem survived the lunar entry environment satisfactorily. The erosion of the heat shield was between 2.5 and 7.6 mm.
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作者: 刺耳    時(shí)間: 2025-3-27 12:40
Book 2006ew the planned lunar landing of a three-man spaceship named Apollo in the mid-1970s. In 1962, it was decided that a specialized vehicle would accompany the main spacecraft, to make the lunar landing while the mothership remained in lunar orbit. To send these vehicles to the Moon would require the de
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作者: Valves    時(shí)間: 2025-3-27 20:18
,Saturn I: Development program 1961–1965,s had required to be shut down, and in that case the vehicle had compensated for its loss. But despite its rapid development and flight record the Saturn I had been overtaken by events and was declared obsolete.
作者: Dysplasia    時(shí)間: 2025-3-27 22:38
AS-201: The first flight of the Saturn IB: a CSM on a ballistic arc 26 February 1966,ome of the flight measurements were corrupted by an electrical short circuit. In order to provide the time to diagnose and rectify the fault in the SPS engine, AS-202 was rescheduled after AS-203, which was to be an S-IVB development flight that would not carry a spacecraft.
作者: Apoptosis    時(shí)間: 2025-3-28 03:21
AS-203: The second flight of the Saturn IB: evaluating the S-IVB 5 July 1966,g coasting flight provided sufficient ullage to maintain the hydrogen settled in its tank, as would be required on a Saturn V dispatching a lunar mission. The simulated restart verified the chilldown and recirculation systems of the J-2 engine. AS-203 was therefore a successful test of the S-IVB sta
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