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

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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


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


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 :
Languages : en
Pages : 25

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 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 :
Languages : en
Pages : 0

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 412

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990

Book Description


Technical Publications Announcements with Indexes

Technical Publications Announcements with Indexes PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556

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


Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196

Book Description