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

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

Evans, R. L.
United States. National Aeronautics and Space Administration.

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

Evaluation of a gravity-simulation technique for studies of man's self-locomotion in lunar environment /

Hewes, Donald E.
Spady, Amos A.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Includes bibliographical references (p. 18)....

Effects of liquid depth on lateral sloshing under weightless conditions /

Salzman, Jack A.
Masica, William J.
Coney, Thom A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 16-17).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

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

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

Effect of throttling on interface behavior and liquid residuals in weightlessness /

Symons, Eugene P.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ac...

Potential problems related to weightlessness and artificial gravity /

Stone, Ralph W.
Piland, William M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 31...

Hydrostatic stability of the liquid-vapor interface in a gravitational field /

Masica, William J.
Otto, Edward W.
Petrash, Donald A.
Lewis Research Center.

Prepared at Lewis Research Center."May 1964"--Cover.Includes bibliographical references (p. 15-16).M...

Zero-gravity equilibrium configuration of liquid-vapor interface in toroidal tanks /

Symons, Eugene P.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Investigating liquid-vapor interface for wetting liquid in toroidal tank during weightlessness.Inclu...

Photographic investigation of liquid behavior on temperature and liquid-vapor sensors used in low-gravity environment /

Berns, James A.
Nussle, Ralph C.
Yeh, Frederick C.
Lewis Research Center.

January 1967

"NASA TM X-1438.""Lewis Research Center, Cleveland, Ohio.""September 1967"--Cover.Includes bibliogra...

EFFECT OF CONTACT ANGLE AND TANK GEOMETRY ON THE CONFIGURATION OF THE LIQUID-VAPOR INTERFACE DURING WEIGHTLESSNESS

Otto, E. W.
Nussle, R. C.
Petrash, D. A.

October 1963

Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid...

Effect of ambient air velocity on atomization of two impinging water jets /

Bittker, David A.
Lewis Research Center.

Prepared at Lewis Research Center."February 1964"--Cover.Includes bibliographical references (p. 15)...

An experimental investigation of the viscous damping of liquid sloshing in spherical tanks /

Sumner, Irving E.
Stofan, Andrew J.
Lewis Research Center.

Prepared at Lewis Research Center."December 1963"--Cover.Includes bibliographical references (p. 11)...

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

Evans, R. L.
United States. National Aeronautics and Space Administration.

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

Evaluation of a gravity-simulation technique for studies of man's self-locomotion in lunar environment /

Hewes, Donald E.
Spady, Amos A.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Includes bibliographical references (p. 18)....

Effects of liquid depth on lateral sloshing under weightless conditions /

Salzman, Jack A.
Masica, William J.
Coney, Thom A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 16-17).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

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

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

Effect of throttling on interface behavior and liquid residuals in weightlessness /

Symons, Eugene P.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10).Mode of ac...

Potential problems related to weightlessness and artificial gravity /

Stone, Ralph W.
Piland, William M.
United States. National Aeronautics and Space Administration.
Langley Research Center.

Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 31...

Hydrostatic stability of the liquid-vapor interface in a gravitational field /

Masica, William J.
Otto, Edward W.
Petrash, Donald A.
Lewis Research Center.

Prepared at Lewis Research Center."May 1964"--Cover.Includes bibliographical references (p. 15-16).M...

Zero-gravity equilibrium configuration of liquid-vapor interface in toroidal tanks /

Symons, Eugene P.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Investigating liquid-vapor interface for wetting liquid in toroidal tank during weightlessness.Inclu...

Photographic investigation of liquid behavior on temperature and liquid-vapor sensors used in low-gravity environment /

Berns, James A.
Nussle, Ralph C.
Yeh, Frederick C.
Lewis Research Center.

January 1967

"NASA TM X-1438.""Lewis Research Center, Cleveland, Ohio.""September 1967"--Cover.Includes bibliogra...

EFFECT OF CONTACT ANGLE AND TANK GEOMETRY ON THE CONFIGURATION OF THE LIQUID-VAPOR INTERFACE DURING WEIGHTLESSNESS

Otto, E. W.
Nussle, R. C.
Petrash, D. A.

October 1963

Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid...

Effect of ambient air velocity on atomization of two impinging water jets /

Bittker, David A.
Lewis Research Center.

Prepared at Lewis Research Center."February 1964"--Cover.Includes bibliographical references (p. 15)...

An experimental investigation of the viscous damping of liquid sloshing in spherical tanks /

Sumner, Irving E.
Stofan, Andrew J.
Lewis Research Center.

Prepared at Lewis Research Center."December 1963"--Cover.Includes bibliographical references (p. 11)...

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

Evans, R. L.
United States. National Aeronautics and Space Administration.

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

Evaluation of a gravity-simulation technique for studies of man's self-locomotion in lunar environment /

Hewes, Donald E.
Spady, Amos A.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Includes bibliographical references (p. 18)....

Effects of liquid depth on lateral sloshing under weightless conditions /

Salzman, Jack A.
Masica, William J.
Coney, Thom A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 16-17).Mode of access: Internet

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

Abstract

Extracted data

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

Abstract

Extracted data

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