J.J. Lombardo

United States Department of Energy

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Gary L. Bennett

Agricultural Research Service

R.W. Englehart

United States Department of Energy

Richard J. Hemler

Lockheed Martin (United States)

J. A. Begley

525 Solutions (United States)

W.J. Eich

Electric Power Research Institute

W.R. Amos

Mound Laser & Photonics Center (United States)

C. W. Whitmore

General Electric (Israel)

R. B. Tatge

General Electric (Israel)

R.W. Zocher

Los Alamos National Laboratory

Alfred Schock

Orbital Systems (Sweden)

Cooperative Institutions

General Electric (United States)

Johns Hopkins University Applied Physics Laboratory

Orbital Systems (Sweden)

Lockheed Martin (United States)

Martin Marietta Materials (United States)

Westinghouse Electric (United States)

The Ohio State University

University of Toronto

Goddard Space Flight Center

General Tire (United States)

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Hydraulic fluid analysis for antenna drive systems

W. J. Logan J.J. Lombardo

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NUCLEAR AND THERMAL CALCULATIONS FOR WCAP-4 IN-PILE EXPERIMENT

A. Bourina W.J. Eich J.J. Lombardo

A description of the nuclear and thermal analysis involved in the design of the WCAP-4 in-pile test is presented. Calculations reveal that no burn-out conditions are expected at the operating fluxes. Calculations of central core temperature and heat output are included. Various hot spot factor calculations for both non-local and local boiling conditions are also given. (J.R.D)

10.2172/4168597

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WCAP-4 IN-PILE TEST LOOP HAZARDS ANALYSIS MANUAL

C.D. Dishman R.P. Goldstein G.H. Eng A. Bournia Ray D. Berringer

From the WCAP-4 in-pile test loop information will be obtained as to how the Yankee fuel pins will withstand the high heat flux of 450,000 Btu/hr-ft/sup 2/ , pressure of 2000 psia, and temperature of 500 to 600 ction prod- F. Possible hazards associated with the operation of WCAP-4 loop experiment in the MTR are presented and each hazard and action taken to minimize or eliminate the hazard are analyzed. (W.D.M.)

Yankee

Hydrostatic test

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Nuclear electric power for space systems: technology background and flight-systems program

Proc., Intersoc. Energy Convers. Eng. Conf.; (United States) (1981)

Gary L. Bennett J.J. Lombardo B.J. Rock

Currently, DOE is developing radioisotope thermoelectric generators (RTGs) for the NASA Galileo mission and the International Solar Polar Mission. This paper surveys past and future uses of RTGs as well as the related dynamic isotope power system (DIPS) which was developed for power levels up to 2 kWe and the space nuclear reactor power plant which will cover the 10- to 100-kWe power range and is in the technology development phase. 7 refs.

Galileo (satellite navigation)

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The dynamic isotope power system: Technology status and demonstration program

Gary L. Bennett J.J. Lombardo

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Nuclear Rocket Design Approach

SAE technical papers on CD-ROM/SAE technical paper series (1970)

Ira Helms J.J. Lombardo

NERVA nuclear rocket engine design technology program, discussing probabilistic techniques for reliability engineering

Rocket (weapon)

10.4271/700801

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Technology Development of Dynamic Isotope Power Systems for Space Applications

Gary L. Bennett J.J. Lombardo

space technology

10.2514/6.1987-9049

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Citations (6)

Cryogenic Radiation Effects on NERVA Structural Materials

ASTM International eBooks (2009)

J.J. Lombardo C.E. Dixon J. A. Begley

Cryogenic radiation tests on structural alloys for NERVA Program, discussing test environment effects

10.1520/stp41340s

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Applications of MHW RTGs for communication satellites

Transactions of the American Nuclear Society (1975)

J.J. Lombardo R. J. Katucki

Communications satellite

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Nuclear rocket materials program

J.J. Lombardo C.W. Funk

to develop the zirconium carbide insulators had been made at the time Rover was terminated. This report details research and development and the experience we gained with both these insulator materials.

Rocket (weapon)

Rocket propellant

10.2172/4203086

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