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
Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Atmosphere Entries with Spacecraft Lift-drag Ratios Modulated to Limit Decelerations
Atmosphere Entries with Vehicle Lift-drag Ration Modulated to Limit Deceleration and Rate of Deceleration
Author: Elliott D. Katzen
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 38
Book Description
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
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).
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
NASA Technical Note
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556
Book Description
Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry
Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description