Proposal for determining the mass of liquid propellant within a space vehicle propellant tank subjected to a zero gravity environment

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Some observations during weightlessness simulation with subject immersed in a rotating water tank /

Stone, Ralph W.
Letko, William.
Langley Research Center.

Prepared at Langley Research Center."September 1964"--Cover.Includes bibliographical references (p. ...

Experimental investigation of liquid surface motion in response to lateral acceleration during weightlessness /

Masica, William J.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 16-17).Mode of access: Internet

Simulator for static liquid configuration in propellant tanks subject to reduced gravity /

Olsen, William A.
United States. National Aeronautics and Space Administration.

Cover title."May 1966."Includes bibliographical references.Mode of access: Internet

An investigation of the liquid level at the wall of a spinning tank

Winch, David M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Fluid mechanics; Propulsion systems, liquid-fuel rockets.Includes bibliogr...

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

An investigation of the response of a scaled model of a liquid-propellant multistage launch vehicle to longitudinal excitation /

Thompson, William M.
United States. National Aeronautics and Space Administration.

Cover title."May 1967."Includes bibliographical references (p. 23).Mode of access: Internet

A thermodynamic analysis of thrust augmentation for nuclear rockets /

Henneberry, Hugh M.
Becker, Roger D.
Corrington, Lester C.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Propulsion systems, liquid fuel rockets; Propulsion systems, nuclear.Inclu...

Influence of weight parameters on the propulsion requirements of orbit-launched vehicles y Dietrich W. Fellenz and Ronald J. Harris.

Fellenz, Dietrich W.
Harris, Ronald J.
United States. National Aeronautics and Space Administration.

Cover title."May 1963."Includes bibliographical references.Mode of access: Internet

Effect of the acceleration disturbances encountered in the MA-7 spacecraft on the liquid-vapor interface in a baffled tank during weightlessness

Petrash, Donald A.
Otto, Edward W.
Nussel, Ralph C.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets

Jack, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1963."Includes bibliographical references.Mode of access: Internet

Effect of surface energy on the liquid-vapor interface configuration during weightlessness

Petrash, Donald A.
Otto, Edward W.
Nelson, Thomas M.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Effect of contact angle and tank geometry on the configuration of the liquid-vapor interface during weightlessness /

Petrash, Donald A.
Otto, Edward W.
Nussle, Ralph C.
Lewis Research Center.

Prepared at Lewis Research Center."October 1963"--Cover.Includes bibliographical references (p. 7).M...

Orbital investigation of propellant dynamics in a large rocket booster /

Buchanan, H.J.
Bugg, F.M.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Slosh dynamics study in near zero gravity : description of vehicle and spacecraft /

Gold, Harold.
Petrash, Donald A.
McArdle, Jack G.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Cover title."May 1967."Includes bibliographical references (p. 26).Mode of access: Internet

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Some observations during weightlessness simulation with subject immersed in a rotating water tank /

Stone, Ralph W.
Letko, William.
Langley Research Center.

Prepared at Langley Research Center."September 1964"--Cover.Includes bibliographical references (p. ...

Experimental investigation of liquid surface motion in response to lateral acceleration during weightlessness /

Masica, William J.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 16-17).Mode of access: Internet

Simulator for static liquid configuration in propellant tanks subject to reduced gravity /

Olsen, William A.
United States. National Aeronautics and Space Administration.

Cover title."May 1966."Includes bibliographical references.Mode of access: Internet

An investigation of the liquid level at the wall of a spinning tank

Winch, David M.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Fluid mechanics; Propulsion systems, liquid-fuel rockets.Includes bibliogr...

Management of cryogenic propellants in a full-scale orbiting space vehicle /

Lacovic, Raymond F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 32).Mode of access: Internet

An investigation of the response of a scaled model of a liquid-propellant multistage launch vehicle to longitudinal excitation /

Thompson, William M.
United States. National Aeronautics and Space Administration.

Cover title."May 1967."Includes bibliographical references (p. 23).Mode of access: Internet

A thermodynamic analysis of thrust augmentation for nuclear rockets /

Henneberry, Hugh M.
Becker, Roger D.
Corrington, Lester C.
United States. National Aeronautics and Space Administration.

Cover title." March 1961."Propulsion systems, liquid fuel rockets; Propulsion systems, nuclear.Inclu...

Influence of weight parameters on the propulsion requirements of orbit-launched vehicles y Dietrich W. Fellenz and Ronald J. Harris.

Fellenz, Dietrich W.
Harris, Ronald J.
United States. National Aeronautics and Space Administration.

Cover title."May 1963."Includes bibliographical references.Mode of access: Internet

Effect of the acceleration disturbances encountered in the MA-7 spacecraft on the liquid-vapor interface in a baffled tank during weightlessness

Petrash, Donald A.
Otto, Edward W.
Nussel, Ralph C.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Feasibility of optimizing nozzle performance for orbital-launch nuclear rockets

Jack, John R.
United States. National Aeronautics and Space Administration.

Cover title."April 1963."Includes bibliographical references.Mode of access: Internet

Effect of surface energy on the liquid-vapor interface configuration during weightlessness

Petrash, Donald A.
Otto, Edward W.
Nelson, Thomas M.
United States. National Aeronautics and Space Administration.

Cover title."January 1963."Includes bibliographical references.Mode of access: Internet

Effect of contact angle and tank geometry on the configuration of the liquid-vapor interface during weightlessness /

Petrash, Donald A.
Otto, Edward W.
Nussle, Ralph C.
Lewis Research Center.

Prepared at Lewis Research Center."October 1963"--Cover.Includes bibliographical references (p. 7).M...

Orbital investigation of propellant dynamics in a large rocket booster /

Buchanan, H.J.
Bugg, F.M.
George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

Slosh dynamics study in near zero gravity : description of vehicle and spacecraft /

Gold, Harold.
Petrash, Donald A.
McArdle, Jack G.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Cover title."May 1967."Includes bibliographical references (p. 26).Mode of access: Internet

Performance of a low-thrust storable propellant rocket at very low chamber pressure /

Wanhainen, John P.
Ross, Phil S.
DeWitt, Richard L.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Propulsion system elements; Propulsion systems, liquid-fuel rockets; Stab...

Some observations during weightlessness simulation with subject immersed in a rotating water tank /

Stone, Ralph W.
Letko, William.
Langley Research Center.

Prepared at Langley Research Center."September 1964"--Cover.Includes bibliographical references (p. ...

Experimental investigation of liquid surface motion in response to lateral acceleration during weightlessness /

Masica, William J.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 16-17).Mode of access: Internet

Proposal for determining the mass of liquid propellant within a space vehicle propellant tank subjected to a zero gravity environment

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Proposal for determining the mass of liquid propellant within a space vehicle propellant tank subjected to a zero gravity environment

Abstract

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