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 |