Fixed-base Simulator Investigation of Lightweight Vehicles for Lunar Escape to Orbit with Kinesthetic Attitude Control and Simplified Manual Guidance PDF Download
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Author: David B. Middleton
Publisher:
ISBN:
Category : Space flight to the moon
Languages : en
Pages : 44
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Book Description
Author: David B. Middleton
Publisher:
ISBN:
Category : Space flight to the moon
Languages : en
Pages : 44
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
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Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1466
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 636
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Book Description
Author: David B. Middleton
Publisher:
ISBN:
Category : Pilot ejection seats
Languages : en
Pages : 44
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Book Description
A fixed-base piloted simulator investigation has been made of the feasibility of using any of several manual guidance and control techniques for emergency lunar escape to orbit with very simplified, lightweight vehicle systems. The escape-to-orbit vehicles accommodate two men, but one man performs all of the guidance and control functions. Three basic attitude-control modes and four manually executed trajectory-guidance schemes were used successfully during approximately 125 simulated flights under a variety of conditions. These conditions included thrust misalinement, uneven propellant drain, and a vehicle moment-of-inertia range of 250 to 12,000 slugs per square foot. Two types of results are presented - orbit characteristics and pilot ratings of vehicle handling qualities.
Author:
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ISBN:
Category :
Languages : en
Pages : 836
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Author:
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ISBN:
Category : Research
Languages : en
Pages : 992
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1008
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 304
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Book Description
Author: Daniel W. Lester
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 544
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