Call Number (LC) Title Results
E 1.99:doe-ne--8312 Multi-phase model development to assess RCIC system capabilities under severe accident conditions 1
E 1.99:DOE/NE/21746--T1 ASME code and ratcheting in piping components. Final technical report 1
E 1.99:doe/ne/32112--t6 Modular Radioisotope Thermoelectric Generator (RTG) Program. Final technical report 1
E 1.99:doe/ne/32115--t1 Special Applications RTG Technology Program Thermoelectric module development summary report. 1
E 1.99:doe/ne/32117-h1 Atomic power in space A history. 1
E 1.99:doe/ne/32123-t1 Development of improved thermoelectric materials for space nuclear power systems. Sixth technical progress report, March 1985 1
E 1.99:doe/ne/32129--t4 NASA low power DIPS [Dynamic Isotope Power System] conceptual design requirements document 1
E 1.99:doe/ne/32134-t1-vol.3-bk.1 Final safety analysis report for the Galileo mission Volume 3 (Book 1), Nuclear risk analysis document. 1
E 1.99:doe/ne/32134-t1-vol.3-bk.2 Final safety analysis report for the Galileo mission Volume 3 (Book 2), Nuclear risk analysis document. 1
E 1.99:doe/ne/32140-20 Users manual for Aerospace Nuclear Safety Program six-degree-of-freedom reentry simulation (TMAGRA6C) 1
E 1.99:doe/ne/32140--21 GPHS motion studies for heat pulse intervals of reentries from gravity-assist trajectories. Aerospace Nuclear Safety Program 1
E 1.99:doe/ne/32140-21 GPHS motion studies for heat pulse intervals of reentries from gravity-assist trajectories. [General Purpose Heat Source Module (GPHS)] 1
E 1.99:doe/ne/32140--22 Follow-up investigations of GPHS motion during heat pulse intervals of reentries from gravity-assist trajectories. Aerospace Nuclear Safety Program 1
E 1.99:doe/ne/32140-22 Follow-up investigations of GPHS motion during heat pulse intervals of reentries from gravity-assist trajectories 1
E 1.99:doe/ne/32170--23 Preliminary reentry safety assessment of the General Purpose Heat Source module for the Cassini mission Aerospace Nuclear Safety Program. 1
E 1.99:doe/ne/32170--24 Reentry response of the lightweight radioisotope heater unit resulting from a Cassini Venus-Venus-Earth-Jupiter gravity assist maneuver accident 1
E 1.99:doe/ne/32180--t1 Nuclear space power safety and facility guidelines study 1
E 1.99:DOE/NE/32181--T1 Space tug applications. Final report 1
E 1.99:doe/ne/32182--t1 Hydrogen permeation resistant heat pipe for bi-modal reactors. Final report, October 1, 1994--September 30, 1995 1
E 1.99:doe/ne/32183--t2 Nuclear thermal rocket plume interactions with spacecraft. Final report 1