Study of the concept of inertially aided barometric altimetry system for supersonic aircraft /

A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development /

Middleton, W. D.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 79-80).Mode of access: Internet

An analysis of terrain bias error in planetary radar altimeters /

Harrington, Richard F.
Stanley, William D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."May 1969"--Cover.Includes bibliographical references (p. 23).Mo...

Eight-level pulse-height analyzer for space physics applications /

Desai, U. D.
Porreca, G.
Van Allen, Roland L.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."January 1961."Cover title.Includes bibliographical referenc...

Study of the concept of inertially aided barometric altimetry system for supersonic aircraft

Ruetenik, J. R.
Thompson, J. H.
Britting, K. R.

June 1971

Study of concept of inertially aided barometric altimetry system to meet vertical separation require...

Optically coupled digital altitude encoder for general aviation altimeters /

Bryant, Floyd R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Studies of optimum body shapes at hypersonic speeds /

Stivers, Louis S., Jr.
Spender, Bernard, Jr.
Langley Research Center.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center and Langley Research Center."N67-40121."Includes bibliographical re...

Altimeter systems survey, final report.

Wright Instruments, inc.
United States. Federal Aviation Agency. Systems Research and Development Service.

"Prepared for the Systems Research and Development Service, Federal Aviation Agency, under contract ...

Parametric study of microwave-powered high-altitude airplane platforms designed for linear flight /

Morris, Charles E. K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 05."November 1981"--Cover."Langley Research Center."Includes bibliographical refere...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Accuracy of aircraft velocities obtained from inertial navigation systems for application to airborne wind measurements /

Rhyne, Richard H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"July 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

A celestial attitude measurement instrument for Project Scanner /

Walsh, T. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1968

Prepared at Langley Research Center."August 1968"--Cover.Includes bibliographical references (p. 14)...

An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane /

Stewart, Eric C.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 44).Mode of ...

Measurement of the maximum altitude attained by the X-15 airplane powered with interim rocket engines /

Stillwell, Wendell H.
Larson, Terry J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft; Piloting; Space vehicles; Vehicle performance.Includes bibliogr...

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development /

Middleton, W. D.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 79-80).Mode of access: Internet

An analysis of terrain bias error in planetary radar altimeters /

Harrington, Richard F.
Stanley, William D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."May 1969"--Cover.Includes bibliographical references (p. 23).Mo...

Eight-level pulse-height analyzer for space physics applications /

Desai, U. D.
Porreca, G.
Van Allen, Roland L.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."January 1961."Cover title.Includes bibliographical referenc...

Study of the concept of inertially aided barometric altimetry system for supersonic aircraft

Ruetenik, J. R.
Thompson, J. H.
Britting, K. R.

June 1971

Study of concept of inertially aided barometric altimetry system to meet vertical separation require...

Optically coupled digital altitude encoder for general aviation altimeters /

Bryant, Floyd R.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ...

Studies of optimum body shapes at hypersonic speeds /

Stivers, Louis S., Jr.
Spender, Bernard, Jr.
Langley Research Center.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Prepared at Ames Research Center and Langley Research Center."N67-40121."Includes bibliographical re...

Altimeter systems survey, final report.

Wright Instruments, inc.
United States. Federal Aviation Agency. Systems Research and Development Service.

"Prepared for the Systems Research and Development Service, Federal Aviation Agency, under contract ...

Parametric study of microwave-powered high-altitude airplane platforms designed for linear flight /

Morris, Charles E. K.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

Subject Category 05."November 1981"--Cover."Langley Research Center."Includes bibliographical refere...

Numerical methods for the design and analysis of wings at supersonic speeds /

Carlson, Harry W.
Miller, David S.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 29-30).Mode ...

Accuracy of aircraft velocities obtained from inertial navigation systems for application to airborne wind measurements /

Rhyne, Richard H.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"July 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

A study of methods which predict supersonic flow fields from body geometry, distance, and Mach number /

Mack, Robert J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 13-14).Mode ...

A celestial attitude measurement instrument for Project Scanner /

Walsh, T. M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1968

Prepared at Langley Research Center."August 1968"--Cover.Includes bibliographical references (p. 14)...

An analytical study and wind-tunnel tests of an aeromechanical gust-alleviation system for a light airplane /

Stewart, Eric C.

January 1976

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 44).Mode of ...

Measurement of the maximum altitude attained by the X-15 airplane powered with interim rocket engines /

Stillwell, Wendell H.
Larson, Terry J.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aircraft; Piloting; Space vehicles; Vehicle performance.Includes bibliogr...

An exploratory study of a parawing as a high-lift device for aircraft /

Naeseth, Rodger L.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development /

Middleton, W. D.
Lundry, J. L., joint author.
United States. National Aeronautics and Space Administration.
Boeing Company.
Langley Research Center.

January 1976

Cover title.Includes bibliographical references (p. 79-80).Mode of access: Internet

An analysis of terrain bias error in planetary radar altimeters /

Harrington, Richard F.
Stanley, William D.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."May 1969"--Cover.Includes bibliographical references (p. 23).Mo...

Eight-level pulse-height analyzer for space physics applications /

Desai, U. D.
Porreca, G.
Van Allen, Roland L.
Goddard Space Flight Center.

Prepared at Goddard Space Flight Center."January 1961."Cover title.Includes bibliographical referenc...

Study of the concept of inertially aided barometric altimetry system for supersonic aircraft /

Abstract

Extracted data

Study of the concept of inertially aided barometric altimetry system for supersonic aircraft /

Abstract

Extracted data

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