Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds /

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

The control of carbon dioxide cryodeposits /

Sharpe, Ellsworth L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 14.Mode of access: Internet

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Entry thermal protection.

Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared under the cognizance of the Langley Research Center.Cover title.Mode of access: Internet

Analytical design of sensors for measuring atmospheric temperature during terminal phase of planetary entry /

Millard, John P.
Sommer, Simon C.
Green, Michael J.
Ames Research Center.

January 1972

Research prepared at Ames Research Center.Cover title.Bibliography: p. 19.Mode of access: Internet

Boundary-layer electron profiles for entry of a blunt slender body at high altitude /

Evans, John S.
Huber, Paul W. (Paul William), 1920-
Schnexnayder, Charles J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 14-15.Mode of access: Internet

Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank /

Sharpe, Ellsworth L.
Jackson, L. Robert.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Heat transfer characteristics of an emergent strand /

Simon, William Emile.
Hedgcoxe, Pat Garner.
Witte, L. C.
Lyndon B. Johnson Space Center.

January 1974

Prepared at Johnson Space Center.Cover title.Includes bibliographical references (p. 33-34).Mode of ...

An experimental investigation of a cold jet emitting from a body of revolution into a subsonic free stream /

Ousterhout, Donald Stewart, 1929-
Langley Research Center.
Old Dominion University. Research Foundation.

January 1972

"Prepared by Old Dominion University Research Foundation ... for Langley Research Center."Cover titl...

Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation /

Schacht, Ralph L.
Quentmeyer, Richard J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 21-22.Mode of access: Internet

Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation /

Quinn, Robert D.
Gong, Leslie.
Dryden Flight Research Facility.

January 1990

Prepared at the Dryden Flight Research Facility.Bibliography: p. 10.Mode of access: Internet

Safeguards applications for isotopic neutron sources /

Beyster, J. Robert, 1924-
Kull, L., joint author.
Brookhaven National Laboratory.
U.S. Atomic Energy Commission.

January 1970

"Prepared for the Office of Safeguards and Materials Management, U.S. Atomic Energy Commission."Bibl...

An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Radiative heat transfer and absorption behind a hypersonic normal shock wave /

Yoshikawa, Kenneth K.
Chapman, Dean R.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

The control of carbon dioxide cryodeposits /

Sharpe, Ellsworth L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 14.Mode of access: Internet

Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles /

Arrington, James P.
Woods, William C.
Langley Research Center.

January 1972

Prepared at Langley Research Center.Cover title.Bibliography: p. 12.Mode of access: Internet

Entry thermal protection.

Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Prepared under the cognizance of the Langley Research Center.Cover title.Mode of access: Internet

Analytical design of sensors for measuring atmospheric temperature during terminal phase of planetary entry /

Millard, John P.
Sommer, Simon C.
Green, Michael J.
Ames Research Center.

January 1972

Research prepared at Ames Research Center.Cover title.Bibliography: p. 19.Mode of access: Internet

Boundary-layer electron profiles for entry of a blunt slender body at high altitude /

Evans, John S.
Huber, Paul W. (Paul William), 1920-
Schnexnayder, Charles J.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 14-15.Mode of access: Internet

Performance of a hypersonic hot fuselage structure with a carbon dioxide frost protected, nonintegral cryogenic tank /

Sharpe, Ellsworth L.
Jackson, L. Robert.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode ...

Heat transfer characteristics of an emergent strand /

Simon, William Emile.
Hedgcoxe, Pat Garner.
Witte, L. C.
Lyndon B. Johnson Space Center.

January 1974

Prepared at Johnson Space Center.Cover title.Includes bibliographical references (p. 33-34).Mode of ...

An experimental investigation of a cold jet emitting from a body of revolution into a subsonic free stream /

Ousterhout, Donald Stewart, 1929-
Langley Research Center.
Old Dominion University. Research Foundation.

January 1972

"Prepared by Old Dominion University Research Foundation ... for Langley Research Center."Cover titl...

Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation /

Schacht, Ralph L.
Quentmeyer, Richard J.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 21-22.Mode of access: Internet

Real-time aerodynamic heating and surface temperature calculations for hypersonic flight simulation /

Quinn, Robert D.
Gong, Leslie.
Dryden Flight Research Facility.

January 1990

Prepared at the Dryden Flight Research Facility.Bibliography: p. 10.Mode of access: Internet

Safeguards applications for isotopic neutron sources /

Beyster, J. Robert, 1924-
Kull, L., joint author.
Brookhaven National Laboratory.
U.S. Atomic Energy Commission.

January 1970

"Prepared for the Office of Safeguards and Materials Management, U.S. Atomic Energy Commission."Bibl...

An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model /

Andrews, Earl H.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Radiative heat transfer and absorption behind a hypersonic normal shock wave /

Yoshikawa, Kenneth K.
Chapman, Dean R.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."September 1962."Cover title.Includes bibliographical references (p...

High-speed flow past wings /

Nørstrud, Helge, 1934-
Langley Research Center.
Lockheed-Georgia Company.

January 1973

"Prepared by Lockheed-Georgia Company ... for Langley Research Center."Cover title.Bibliography: p. ...

A study for development of aerothermodynamic test model materials and fabrication technique /

Dean, W. G.
Connor, L. E.
Langley Research Center.
Lockheed Missiles and Space Company.

January 1972

"Prepared by Lockheed Missiles & Space Company ... for Langley Research Center."Cover title.Bibliogr...

The control of carbon dioxide cryodeposits /

Sharpe, Ellsworth L.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Bibliography: p. 14.Mode of access: Internet

Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds /

Abstract

Extracted data

Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds /

Abstract

Extracted data

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