Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry PDF Download
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Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
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Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
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Author: Lionel L. Levy
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ISBN:
Category :
Languages : en
Pages : 0
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Author: Lionel L. Levy (Jr., & Elliott D. Katzen)
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Category :
Languages : en
Pages :
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Author: LIONEL L. JR. LEVY
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Category :
Languages : en
Pages : 1
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ATMOSPHERE ENTRY TRAJECTORIES WERE STUDIED TO DETERMINE THE RANGE FOR TWO TYPES OF MANEUVERS. For one type range was controlled principally by varying the point in the trajectory where the lift-drag ratio was reduced to maximum negative lift-drag ratio. For the other maneuver range was controlled principally by varying the value to which the lift-drag ratio was reduced. The influence on range of maximum deceleration limit and an error in lift-drag ratio were included; the convective and radative heating to the stagnation point of the spacecraft were also studied. The analysis was made for a spacecraft with a maximum lift-drag ratio of 0.5 entering the earth's atmosphere at parabolic velocity. The results for both types of maneuvers indicate that the spacecraft aerodynamics can provide range up to global range.
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Category :
Languages : en
Pages : 418
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![Space Rendez[v]ous, Rescue and Recovery PDF](https://books.google.com/books/content/images/frontcover/RqUmAQAAMAAJ?fife=w80-h100)
Author: Defense Documentation Center (U.S.)
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ISBN:
Category : Astronautics
Languages : en
Pages : 128
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 172
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Author:
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Category : Government publications
Languages : en
Pages : 1990
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 826
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Author: United States. Superintendent of Documents
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Category : United States
Languages : en
Pages : 1284
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