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Displaying 21—30 of 1000 matches for query "A_Survey_Of_Various_Vehicle_Systems_For_The_Manned_Lunar_Landing_1961" retrieved in 0.058 sec with these stats:
- "a" found 169938 times in 18149 documents
- "survey" found 1708 times in 1097 documents
- "of" found 295472 times in 20552 documents
- "various" found 1803 times in 1215 documents
- "vehicl" found 10011 times in 4664 documents
- "system" found 26638 times in 8217 documents
- "for" found 102366 times in 17182 documents
- "the" found 506431 times in 20587 documents
- "man" found 10979 times in 4195 documents
- "lunar" found 12612 times in 4514 documents
- "land" found 10467 times in 4286 documents
- "1961" found 12306 times in 1330 documents
... A survey of ... of Victoria, Centre for Aerospace Research, May 2014.
18 Gomes, R., “Development of a reliable and low-cost miniaturized reaction wheel system for CubeSat applications,” Canadian Space Summit, 2015.
An Accurate, Inexpensive Attitude Determination and Control System for ...
... FOR THE STARS'''
by Bergaust, E.
''New York, 1960: Doubleday and Co., Inc., 407 pages, $4.95''
A biography of Dr. Wernher von Braun, the book is written in a ...
... of Pages''' - 12
Abstract
For the past 45 years the red planet has been the focus of human space exploration. Commencing with the crash landing of Mars 2 some 35 years ago, humanity has left a range of traces on the Martian ... overview of the successful landing missions and the material culture these missions deposited on the surface of Mars. Environmental conditions on Mars are also considered, as these differ from those of the Earth, and have important implications for the future ...
... version of the B-dot control law using magnetic torquers is implemented for the detumbling stage. A 3-axis sliding mode controller is employed for the nominal, Earth-tracking mission phase, using a specially designed reaction wheel system (RWS). A momentum dumping system using the magnetic torquers is also devised to ensure that the RWS does not reach saturation. Simulations are performed in an environment for the ECOSat-III cube satellite: a nanosatellite designed by the University of ...
... a maximum torque of 8.3125 × 10−6 Nm and is targeted for a lifetime of two years.
An Accurate, Inexpensive Attitude Determination and Control System for ...
... for ballistic vehicles, reentry and recovery, auxiliary subsystems, and the missile as an integrated vehicle system.
Extracted from the 1962 Publication ''Annotated Bibliography of Space Science and Technology with an Astronomical Supplement - A History of Astronautical Book Literature 1931 - 1961 ...
... a system is, of course, the responsibility of leadership, beginning not only with the NASA Administrator, but also with the President, the Congress, and also with the roots of this tree, the American people themselves. We all bear some responsibility for the ...
... _011509155026.pdf Lunar Landing Training Vehicle Service and Maintenance Manual Prt 1 (19MB PDF)
Media:LunarLandTrain2_011509155036.pdf Lunar Landing Training Vehicle Service and Maintenance Manual Prt 2 (16MB PDF)
Media:LunarLandTrain3_011509155044.pdf Lunar Landing Training Vehicle Service and Maintenance Manual Prt 3 (13MB PDF)
Media:LunarLandTrain4_011509155052.pdf Lunar Landing Training Vehicle Service ...
... the mix are various considerations of the number of spaceflight participants per flight, the economic viability of stringent safety standards, the plethora of possible flight vehicles and the compensation mechanism in case of violations of safety regulations. This paper surveys the legal challenges in the regulation of ...
... SYSTEMS FOR MISSILES AND SPACE VEHICLES'''
by Brown, K. and P. Weiser
''New York, 1961: McGraw-Hill Book Co., Inc., 490 pages, $15.00''
The book provides engineers with an understanding of the ...
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