Ask
Search
My library

About
Statistics
Contact
Data Protection
Accessibility
Imprint
Changelog
Frontend: v1.31.3
Backend: v1.11.4

We use cookies to provide a better user experience.

Data Protection

Angle-of-attack analysis for Project Fire 1 payload reentry flight

Woodbury, G. E.

Publication date

April 1966

Language

English

Abstract

Computer program for Project Fire 1 payload reentry flight angle of attack analysi

Extracted data

Related items

Study of flow fields about axisymmetric blunt bodies at large angle-of-attack Final report

October 1965

Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...

Flight Analysis of a Suborbital Space Probe: the Light Airbag-Protected Lander

Sund, Erik

January 2010

A novel Inatable Aerodynamic Decelerator (IAD) and platform for multi-pointmeasurements in the ionos...

Analysis of flight data from a High-Incidence Research Model by system identification methods

Klein, Vladislav
Batterson, James G.

November 1989

Data partitioning and modified stepwise regression were applied to recorded flight data from a Royal...

Angle-of-attack analysis of a spinning slender cone with slight aerodynamic and mass asymmetries /reentry F/

Woodbury, G. E.
Morris, W. D.

September 1970

Angle of attack analysis of spinning slender reentry cone with slight aerodynamic and mass asymmetri...

Angle-of-attack analysis for Project Fire 1 payload reentry flight /

Woodbury, Gerard E.
Langley Research Center.

Prepared at Langley Research Center."April 1966"--Cover.Includes bibliographical references (p. 25)....

Project fire integrated post flight evaluation report, flight no. 1

October 1964

Fire project flight test of Atlas launch vehicle, Antares velocity package, and reentry vehicl

Flow field prediction and analysis, project fire final report

Nicolet, W. E.
Buckingham, A. C.
Hoshizaki, H.
Vinokur, M.

March 1965

Flow field, and convective and radiative heating predictions for NASA Fire project reentry package t...

Analysis of the project fire re-entry package flow field final technical report

Foster, R. M.
Kuby, W. C.
Holt, M.
Hoglund, R. F.
Byron, S. R.

October 1964

Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at h...

Operating experiences of retardant bombers during firefighting operations

Morris, G. J.
Avery, D. E.
Jewel, J. W., Jr.

November 1974

Data are presented on operational practices and maneuver accelerations experienced by two Douglas DC...

Flight evaluation of angle of attack as a control parameter in general-aviation aircraft

Gaidsick, H. G.
Gee, S. W.
Enevoldson, E. K.

March 1971

Investigation of angle of attack information display for pilots to increase efficiency of general av...

Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flight

Moes, Timothy R.
Whitmore, Stephen A.

February 1991

A technique was developed to improve the fidelity of airdata measurements during dynamic maneuvering...

Internal velocity factors

Massaglia, J. L.
Frank, A. J.
Cathcart, J. R.

November 1968

Computer program analyzes the entries and planetary trajectories of space vehicles. It obtains the e...

Development of Advanced Methods of Trajectory and Structural Analysis for Hypersonic Aircraft

Ardema, Mark D.

March 1997

The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...

Entry trajectory, entry environment, and analysis of spacecraft motion for the RAM C-3 flight experiment

Weaver, W. L.
Bowen, J. T.

June 1972

The RAM C-3 flight experiment was launched to study the problem of radiofrequency blackout at an ent...

Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the Space Shuttle from Mach 8 to 1.5

Stone, H. W.
Powell, R. W.

January 1985

A six degree of freedom simulation analysis was performed for the space shuttle orbiter during entry...

Study of flow fields about axisymmetric blunt bodies at large angle-of-attack Final report

October 1965

Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...

Flight Analysis of a Suborbital Space Probe: the Light Airbag-Protected Lander

Sund, Erik

January 2010

A novel Inatable Aerodynamic Decelerator (IAD) and platform for multi-pointmeasurements in the ionos...

Analysis of flight data from a High-Incidence Research Model by system identification methods

Klein, Vladislav
Batterson, James G.

November 1989

Data partitioning and modified stepwise regression were applied to recorded flight data from a Royal...

Angle-of-attack analysis of a spinning slender cone with slight aerodynamic and mass asymmetries /reentry F/

Woodbury, G. E.
Morris, W. D.

September 1970

Angle of attack analysis of spinning slender reentry cone with slight aerodynamic and mass asymmetri...

Angle-of-attack analysis for Project Fire 1 payload reentry flight /

Woodbury, Gerard E.
Langley Research Center.

Prepared at Langley Research Center."April 1966"--Cover.Includes bibliographical references (p. 25)....

Project fire integrated post flight evaluation report, flight no. 1

October 1964

Fire project flight test of Atlas launch vehicle, Antares velocity package, and reentry vehicl

Flow field prediction and analysis, project fire final report

Nicolet, W. E.
Buckingham, A. C.
Hoshizaki, H.
Vinokur, M.

March 1965

Flow field, and convective and radiative heating predictions for NASA Fire project reentry package t...

Analysis of the project fire re-entry package flow field final technical report

Foster, R. M.
Kuby, W. C.
Holt, M.
Hoglund, R. F.
Byron, S. R.

October 1964

Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at h...

Operating experiences of retardant bombers during firefighting operations

Morris, G. J.
Avery, D. E.
Jewel, J. W., Jr.

November 1974

Data are presented on operational practices and maneuver accelerations experienced by two Douglas DC...

Flight evaluation of angle of attack as a control parameter in general-aviation aircraft

Gaidsick, H. G.
Gee, S. W.
Enevoldson, E. K.

March 1971

Investigation of angle of attack information display for pilots to increase efficiency of general av...

Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flight

Moes, Timothy R.
Whitmore, Stephen A.

February 1991

A technique was developed to improve the fidelity of airdata measurements during dynamic maneuvering...

Internal velocity factors

Massaglia, J. L.
Frank, A. J.
Cathcart, J. R.

November 1968

Computer program analyzes the entries and planetary trajectories of space vehicles. It obtains the e...

Development of Advanced Methods of Trajectory and Structural Analysis for Hypersonic Aircraft

Ardema, Mark D.

March 1997

The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...

Entry trajectory, entry environment, and analysis of spacecraft motion for the RAM C-3 flight experiment

Weaver, W. L.
Bowen, J. T.

June 1972

The RAM C-3 flight experiment was launched to study the problem of radiofrequency blackout at an ent...

Effect of aerodynamic and angle-of-attack uncertainties on the May 1979 entry flight control system of the Space Shuttle from Mach 8 to 1.5

Stone, H. W.
Powell, R. W.

January 1985

A six degree of freedom simulation analysis was performed for the space shuttle orbiter during entry...

Study of flow fields about axisymmetric blunt bodies at large angle-of-attack Final report

October 1965

Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...

Flight Analysis of a Suborbital Space Probe: the Light Airbag-Protected Lander

Sund, Erik

January 2010

A novel Inatable Aerodynamic Decelerator (IAD) and platform for multi-pointmeasurements in the ionos...

Analysis of flight data from a High-Incidence Research Model by system identification methods

Klein, Vladislav
Batterson, James G.

November 1989

Data partitioning and modified stepwise regression were applied to recorded flight data from a Royal...