Gas flow, emittance, and ion current capabilities of porous thungsten /

An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 /

Vick, Allen R.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Propulsion system elements.Includes bibliographical references....

An optimization of powerplant paramemters for orbital-launch nuclear rockets /

Johnson, Paul G.
Smith, Roger L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Propulsion systems, nuclear.Includes bibliographical references.Mode of ...

Satellite and space propulsion systems /

Moeckel, Wolfgang E.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 28-29).Mode of access: Internet

A comparison of reverse-feed and porous-tungsten ion engines

Reynolds, Thaine W.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical r...

Theoretical performance of propellants suitable for electrothermal jet engines /

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

Cover title." April 1961."Propellants; Propulsioin systems, electric; Propulsion systems, theory.Inc...

Evaluation of a hollow, cylindrical, contact-ion source/

Kotnik, J. Thomas
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Propulsion systems, electric.Includes bibliographical references.Mode of...

The design and operation of a continuous flow electrodeless plasma accelerator /

Barger, Raymond L.
Beasley, William D.
Brooks, Joseph D.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Propulsion systems, electric.Includes bibliographical references.Mode of...

An ion rocket with an electron-bombardment ion source /

Kaufman, Harold R.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Fluid mechanics; Propulsion systems, electric.Includes bibliographical re...

Comparative measurements of beam power in ion-rocket research. /

Dangle, E. E.
Baldwin, L. V.
Sandborn, V. A.
Richley, E. A.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Fluid mechanics; Propulsion systems, electric.Includes bibliographical refere...

Accelerator grid tests on an electron-bombardment ion rocket

Kerslake, William R.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical r...

Performance evaluation of a mercury-propellant feed system for a flight-model ion engine /

Pawlik, Eugene V.
Wenger, Norman C.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Propulsion systems, electric; Stability and control.Includes bibliographical...

Investigation of a 10-centimeter-diameter electron-bombardment ion rocket

Reader, Paul D.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical re...

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...

A parametric study of the thermionic diode system for large nuclear-electric powerplants in space vehicles /

Bernatowicz, Daniel T.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Power sources, supplementary; Propulsion systems, electric; Propulsion sy...

Two-dimensional ion beams with small lateral spreading /

Mirels, Harold.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsion systems, electric; Space vehicles.Includes bibl...

An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 /

Vick, Allen R.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Propulsion system elements.Includes bibliographical references....

An optimization of powerplant paramemters for orbital-launch nuclear rockets /

Johnson, Paul G.
Smith, Roger L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Propulsion systems, nuclear.Includes bibliographical references.Mode of ...

Satellite and space propulsion systems /

Moeckel, Wolfgang E.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 28-29).Mode of access: Internet

A comparison of reverse-feed and porous-tungsten ion engines

Reynolds, Thaine W.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical r...

Theoretical performance of propellants suitable for electrothermal jet engines /

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

Cover title." April 1961."Propellants; Propulsioin systems, electric; Propulsion systems, theory.Inc...

Evaluation of a hollow, cylindrical, contact-ion source/

Kotnik, J. Thomas
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Propulsion systems, electric.Includes bibliographical references.Mode of...

The design and operation of a continuous flow electrodeless plasma accelerator /

Barger, Raymond L.
Beasley, William D.
Brooks, Joseph D.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Propulsion systems, electric.Includes bibliographical references.Mode of...

An ion rocket with an electron-bombardment ion source /

Kaufman, Harold R.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Fluid mechanics; Propulsion systems, electric.Includes bibliographical re...

Comparative measurements of beam power in ion-rocket research. /

Dangle, E. E.
Baldwin, L. V.
Sandborn, V. A.
Richley, E. A.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Fluid mechanics; Propulsion systems, electric.Includes bibliographical refere...

Accelerator grid tests on an electron-bombardment ion rocket

Kerslake, William R.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical r...

Performance evaluation of a mercury-propellant feed system for a flight-model ion engine /

Pawlik, Eugene V.
Wenger, Norman C.
United States. National Aeronautics and Space Administration.

Cover title."June 1962."Propulsion systems, electric; Stability and control.Includes bibliographical...

Investigation of a 10-centimeter-diameter electron-bombardment ion rocket

Reader, Paul D.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Fluid mechanics; Propulsion systems, electric.Includes bibliographical re...

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...

A parametric study of the thermionic diode system for large nuclear-electric powerplants in space vehicles /

Bernatowicz, Daniel T.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Power sources, supplementary; Propulsion systems, electric; Propulsion sy...

Two-dimensional ion beams with small lateral spreading /

Mirels, Harold.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Fluid mechanics; Propulsion systems, electric; Space vehicles.Includes bibl...

An investigation to determine the discharge and thrust characteristics of auxiliary-air outlets for a stream Mach number of 3.25 /

Vick, Allen R.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft; Propulsion system elements.Includes bibliographical references....

An optimization of powerplant paramemters for orbital-launch nuclear rockets /

Johnson, Paul G.
Smith, Roger L.
United States. National Aeronautics and Space Administration.

Cover title."February 1961."Propulsion systems, nuclear.Includes bibliographical references.Mode of ...

Satellite and space propulsion systems /

Moeckel, Wolfgang E.

January 1960

"June 1960."Cover title.Includes bibliographical references (p. 28-29).Mode of access: Internet

Gas flow, emittance, and ion current capabilities of porous thungsten /

Abstract

Extracted data

Gas flow, emittance, and ion current capabilities of porous thungsten /

Abstract

Extracted data

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