Atmosphere Entries with Vehicle Lift-drag Ration Modulated to Limit Deceleration and Rate of Deceleration PDF Download

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Atmosphere Entries with Vehicle Lift-drag Ration Modulated to Limit Deceleration and Rate of Deceleration

Atmosphere Entries with Vehicle Lift-drag Ration Modulated to Limit Deceleration and Rate of Deceleration PDF Author: Elliott D. Katzen
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 38

Book Description


Atmosphere Entries with Vehicle Lift-drag Ration Modulated to Limit Deceleration and Rate of Deceleration

Atmosphere Entries with Vehicle Lift-drag Ration Modulated to Limit Deceleration and Rate of Deceleration PDF Author: Elliott D. Katzen
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 38

Book Description


Atmosphere Entries with Vehicle Lift-drag Ratio Modulated to Limit Deceleration and Rate of Deceleration - Vehicles with Maximum Lift-drag Ratio of 0.5

Atmosphere Entries with Vehicle Lift-drag Ratio Modulated to Limit Deceleration and Rate of Deceleration - Vehicles with Maximum Lift-drag Ratio of 0.5 PDF Author: Elliott D. Katzen
Publisher:
ISBN:
Category :
Languages : en
Pages : 1

Book Description
An analysis has been made of atmosphere entries for which the vehicle lift-drag ratio was modulated to maintain specified maximum decelerations and/or maximum deceleration rates. The part of the vehicle drag polar used during modulation was from maximum lift coefficient to minimum drag coefficient. The entries were at parabolic velocity and the vehicle maximum lift-drag ratio was 0.5. Two-dimensional trajectory calculations were made for a nonrotating, spherical earth with an exponential atmosphere. The results of the analysis indicate that for a given initial flight-path angle, modulation generally resulted in a reduction of the maximum deceleration to 60% of the unmodulated value or a reduction of maximum deceleration rate to less than 50% of the unmodulated rate. These results were equivalent, for a maximum deceleration of 10g, to lowering the undershoot boundary 24 miles with a resulting decrease in total convective heating to the stagnation point of 22%. The maximum convective heating rate was increased 18%. (Author).

Atmosphere Entries with Spacecraft Lift-drag Ratios Modulated to Limit Decelerations

Atmosphere Entries with Spacecraft Lift-drag Ratios Modulated to Limit Decelerations PDF Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 440

Book Description


The Use of Drag Modulation to Limit the Rate at which Deceleration Increases During Nonlifting Entry

The Use of Drag Modulation to Limit the Rate at which Deceleration Increases During Nonlifting Entry PDF Author: Lional L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

Book Description


The Variation and Control of Range Traveled in the Atmosphere by a High-drag Variable-lift Entry Vehicle

The Variation and Control of Range Traveled in the Atmosphere by a High-drag Variable-lift Entry Vehicle PDF Author: Donald C. Cheatham
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 50

Book Description


Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry

Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry PDF Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24

Book Description


Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
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Index of NASA Technical Publications

Index of NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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Category : Aeronautics
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Monthly Catalog of United States Government Publications

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ISBN:
Category : Government publications
Languages : en
Pages : 1284

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