1 | S. B. Rawlins, D. L. Dale Thomas | A PROPOSED SOLUTION TO ADDRESS NUCLEAR THERMAL PROPULSION FUEL EMBRITTLEMENT AND CRYOGENIC HYDROGEN REQUIREMENTS |
2 | D. Nikitaev | AIR AND SPACE THERMAL ROCKET ENGINE WITH TURBOJET (ASTRET) |
3 | T. Cwik, W. Zimmerman, M. Smith | AN ARCHITECTURE FOR A NUCLEAR POWERED CRYOBOT TO ACCESS THE OCEANS OF ICY WORLDS |
4 | A. Austin | AN EXPLORATION OF MISSION CONCEPTS THAT COULD UTILIZE SMALL RPS |
6 | G. Romanoski | AN INVESTIGATION OF THE RHEOLOGICAL BEHAVIOR OF PHENOLIC RESINS CONSIDERED FOR PRODUCTION OF CARBON BONDED CARBON FIBER INSULATION |
7 | R. M. Wham, R. Steve Owens, J. H. Miler, S. Pierce | AUTOMATION OF NEPTUNIUM OXIDEALUMINUM TARGET FABRICATION |
8 | D. K. Bond, B. Goddard, S. Bilbao Y. Leon, R. C. Singleterry, Jr. | COMPARING THE EFFECTIVENESS OF POLYMER AND COMPOSITE MATERIALS TO ALUMINUM FOR EXTENDED DEEP SPACE TRAVEL |
10 | C. Wang | CONCEPTUAL DESIGN OF A MICRO NUCLEAR REACTOR POWER SOURCE FOR MULTI-APPLICAITON |
11 | J. N. Easley, C. Denbrock | CONSIDERATIONS FOR CLOSED-LOOP BRAYTON POWER CYCLE FOR NUCLEAR THERMAL ROCKET WITH DECAY HEAT |
12 | L. Carasik, M. Eades, V. Patel | DECAY HEAT STUDIES TO REDUCE ACTIVE COOLING TIME OF A NUCLEAR THERMAL PROPULSION SYSTEM |
13 | J. Mcduffee | DESIGN AND ANALYSIS OF A NPO2 TARGET FOR THE PRODUCTION OF PU238 |
14 | J. Hong, K. Son, J. Kim, J. Kim | DESIGN OF ETG FOR LOW ORBIT TEST OF THE KOREA LAUNCH VEHICLE |
15 | C. Daily | DESIGN OPTIMIZATION STUDIES FOR NPO2 TARGETS IRRADIATED IN THE HIGH FLUX ISOTOPE REACTOR |
16 | Z. Li, M. Lang, J. Sun, L. Shi | DEVELOPMENT OF A SYSTEM ANALYSIS CODE FOR NUCLEAR THERMAL ROCKET ENGINE |
17 | A. P. Shivprasad | DEVELOPMENT OF SINTERED YTTRIUM DIHYDRIDE COMPACTS FOR NUCLEAR REACTOR MODERATOR APPLICATIONS |
18 | A. | DEVELOPMENT OF THE PLUTONIUM MODELING AND ASSESSMENT (PUMA) SIMULATION THROUGH THE COUPLING OF EXPERIMENTS AND MOLECULAR DYNAMICS |
19 | S. Oriti | DYNAMIC RPS PATH TO FLIGHT |
20 | J. Locke, B. Lal | EMERGENCE OF A COMMERCIAL SPACE NUCLEAR ENTERPRISE |
21 | C. E. Whiting, D. P. Kramer, C. D. Barklay | EMPIRICAL POWER PREDCITION FOR MMRTG F1 |
22 | N. Gallego | EVALUATION OF ALTERNATIVE FIBERS TO REPLACE NARC-RAYON FOR THE PRODUCTION OF CBCF |
23 | S. Judd | EXPERIMENTALLY VERIFYING THE EFFECTIVENESS OF FUELED CONTROL DRUMS |
24 | M. A. White | FLEXURE ISOTOPE STIRLING CONVERTOR (FISC) DEVELOPMENT PROGRESS |
25 | M. Stewart | FUEL ELEMENT TO MODERATOR ELEMENT HEAT TRANSFER ANALYSIS |
26 | B. Makenas, D. Wootan | HANFORD'S ROLE IN SPACE POWER |
27 | S. Whalen | HIGH PERFORMANCE LIGHTWEIGHT MATERIALS MADE BY SHEAR ASSISTED PROCESSING AND EXTRUSION (SHAPE) |
28 | X. Chunyang, X. Jiachun | HISTORY AND CHALLENGES OF SPACE NUCLEAR REACTOR POWER SYSTEMS |
29 | T. G. Duffin, K. M. Benensky, S. J. Zinkle, M. W. Barnes | HOT HYDROGEN TESTING AND MICROSTRUCTURAL CHARACTERIZATION OF MOLYBDENUM CERMETS FOR NUCLEAR THERMAL PROPULSION |
30 | B. Taylor | HYBRID FUEL COUPLING IN A PULSED Z-PINCH ROCKET ENGINE |
31 | J. Teague | IMPACT TEMPERATURE DETERMINATION FOR GPHS SAFETY TESTING |
32 | J. F. Zakrajsek, T. Sutliff, J. Hamley, C. Sandifer, P. Mccallum, T. Bishop, M. Mccune | IMPLEMENTATION OF CROSS-AGENCY NUCLEAR APPLICATIONS |
33 | P. Mccallum | IMPROVING THE NUCLEAR LAUNCH APPROVAL PROCESS; PROGRESS AND PLANS |
34 | D. Chandler, M. W. Crowell, K. E. Royston | INCREASED PLUTONIUM-238 PRODUCTION VIA HIGH FLUX ISOTOPE REACTOR PERMANENT BERYLLIUM REFLECTOR REDESIGN |
35 | K. G. Myhre, M. E. Woods, A. J. Unger, P. D. Benny, D. E. Benker, E. D. Collins, L. H. Delmau, D. W. Depaoli, F. D. Riley, R. M. Wham | INITIAL TESTING OF MEDIATED ELECTROCHEMICAL OXIDATION FOR INCLUSION IN THE PLUTONIUM-238 PRODUCTION PROGRAM |
36 | J. Zillinger, B. Segel, K. Benensky, D. Tucker, M. Barnes | INVESTIGATION OF PRODUCTION PARAMETER EFFECTS ON SPARK PLASMA SINTERED MOLYBDENUM CERMET WAFERS FOR NUCLEAR THERMAL PROPULSION APPLICATIONS |
37 | D. Lonnie Johnson | JOHNSON THERMO-ELECTROCHEMICAL CONVERTER (JTEC) AS A HEAT TO ELECTRIC GENERATOR FOR NUCLEAR POWER SYSTEMS |
38 | P. Mcclure | KILOPOWER - MAXIMUM CREDIBLE DOSE FOR A CRITICALITY ACCIDENT |
39 | P. Mcclure | KILOPOWER - MAXIMUM CREDIBLE FISSIONS FOR A CRITICALITY ACCIDENT |
40 | D. I. Poston | KILOPOWER REACTORS FOR POTENTIAL SPACE EXPLORATION MISSIONS |
41 | C. Russell Joyner | LEU NTP ENGINE SYSTEM TRADES AND MISSION OPTIONS |
42 | C. J. Romnes, D. E. Chavez, B. J. Martinez, N. M. Osterhaus, W. R. Ford, R. Lenard | LOW ENRICHED URANIUM NUCLEAR THERMAL ROCKET DESIGN INSPIRED BY THE SPACE NUCLEAR THERMAL PROPULSION PROJECT |
43 | B. Sondelski | MASS OPTIMIZATION OF POWER SYSTEM FOR SPACE APPLICATIONS |
44 | S. Wilson, S. Oriti | MATURATION OF DYNAMIC POWER CONVERTORS FOR RADIOISOTOPE POWER SYSTEMS |
45 | W. Carpenter, K. Benensky, M. Barnes, D. Dennis Tucker | MICROSTRUCTURAL EVOLUTION OF HIGH DENSITY W-CERMETS EXPOSED TO FLOWING HYDROGEN AT TEMPERATURES EXCEEDING 2000 K |
46 | D. Kramer | MIXED ALUMINA/CERIA COMPOSITIONS AS AN ENHANCED CERAMIC PROCESSING SURROGATE FOR RPS FUEL PELLETS |
47 | L. Hawkins | MODELING HELIUM AND OXYGEN BEHAVIOR OF A PLUTONIA PELLET IN AN MMRTG |
48 | A. Denig, M. Eades | MONTE CARLO-INFORMED DECAY HEAT MODEL FOR CERMET LEU-NTP SYSTEMS |
49 | D. Kramer | NUCLEAR HEAT SOURCE CONSIDERATIONS FOR AN ICY MOON EXPLORATION SUBSURFACE PROBE |
50 | K. Kowal | NUCLEAR LAUNCH APPROVAL: OPTIONS FOR CRITERIA |
51 | S. S. Voss | NUCLEAR SECURITY CONSIDERATIONS FOR SPACE NUCLEAR POWER: A REVIEW OF PAST PROGRAMS WITH RECOMMENDATIONS FOR FUTURE CRITERIA |
52 | J. Rader, M. B. R. Smith, M. Scott Greenwood, T. Jay Harrison | NUCLEAR THERMAL PROPULSION DYNAMIC MODELING WITH MODELICA |
53 | D. Sikorski | NUCLEAR THERMAL ROCKET CONTROL |
54 | R. S. Raju, J. E. Foster | OVERVIEW AND FUTURE OF OPEN CYCLE GAS-CORE NUCLEAR ROCKET |
55 | R. Howard | OVERVIEW OF THE PLUTONIUM-238 SUPPLY PROGRAMS CERMET PRODUCTION TARGET |
56 | Y. Ji | PARAMETRIC STUDY ON THERMAL HYDRAULICS CHARACTERISTICS OF A PARTICLE BED REACTOR FOR NUCLEAR THERMAL PROPULSION |
57 | F. Anne Carver | PARTICLE SIZE ANALYSIS OF CERIUM DIOXIDE SURROGATE MATERIALS AS A SIMULANT FOR PLUTONIUM-238 DIOXIDE FUELS PROCESSING |
58 | T. Winkle | PASSIVE AND ACTIVE COOLING ANALYSIS FOR DECAY HEAT OF NUCLEAR THERMAL PROPULSION SYSTEMS |
59 | J. Rock | PATH TO A NEXT GENERATION RADIOISOTOPE THERMOELECTRIC GENERATOR (RTG) |
60 | S. V. Howieson, J. Behrens, K. M. Kowal | POTENTIAL LAUNCH APPROVAL PROCESS FOR COMMERCIAL SPACE NUCLEAR SYSTEMS |
61 | D. Depaoli | PROCESS DEVELOPMENT FOR PLUTONIUM-238 PRODUCTION AT OAK RIDGE NATIONAL LABORATORY |
62 | R. Miller, B. Friske, K. R. Veach, Jr | QUALIFICATION OF SPECIAL PROCESSES USING A GRADED APPROACH FOR THE LIGHT-WEIGHT RADIOISOTOPE HEATER UNIT METALLIC COMPONENT PRODUCTION AT OAK RIDGE NATIONAL LABORATORY |
63 | G. Bruder, F. Ritzert | RADIOISOTOPE POWER GENERATION WITH THERMOACOUSTIC POWER SYSTEM (TAPS) TECHNOLOGY |
64 | T. J. Sutliff | RADIOISOTOPE POWER SYSTEMS - AN INTERAGENCY PROGRAM STATUS |
65 | K. Rex Veach, Jr. | RE-ESTABLISHMENT OF LIGHT-WEIGHT RADIOISOTOPE HEATER UNIT PLATINUM-30% RHODIUM ALLOY COMPONENTS PRODUCTION AT OAK RIDGE NATIONAL LABORATORY |
66 | A. Camp, A. Klein, P. Mcclure, P. Mccallum, S. Voss | RECOMMENDATIONS FOR THE NUCLEAR SAFETY AND LAUNCH APPROVAL PROCESS FOR FISSION REACTORS |
67 | D. I. Poston | RESULTS OF THE KRUSTY NUCLEAR SYSTEM TEST |
68 | D. I. Poston | RESULTS OF THE KRUSTY WARM CRITICAL EXPERIMENTS |
69 | N. D. Gaffin, S. J. Zinkle, K. M. Benensky | REVIEW OF IRRADIATION HARDENING AND EMBRITTLEMENT EFFECTS IN REFRACTORY METALS RELEVANT TO NUCLEAR THERMAL PROPULSION APPLICATIONS |
70 | M. Krecicki | SENSITIVITY STUDIES OF THE TUNGSTEN VECTOR ON THE PERFORMANCE OF A LEU NTP ENGINE |
72 | J. Stephen Herring, S. Mackwell, C. Pestak, K. Hilser | SMALL MODULAR FISSION REACTORS FOR SPACE APPLICATIONS: ENABLING AN AFFORDABLE, COMMERCIALLY DEVELOPED POWER ARCHITECTURE FOR THE MOON AND BEYOND |
73 | V. Patel | SNRE EIGENVALUE UNCERTAINTY QUANTIFICATION FROM NUCLEAR DATA SOURCES |
74 | J. R. Casani | SPACE FISSION POWER: NASAS BEST BET TO CONTINUE TO EXPLORE THE OUTER SOLAR SYSTEM |
75 | D. Wootan, B. Makenas | SPACE POWER TESTING IN THE FAST FLUX TEST FACILITY |
76 | J. Collins, J. Gary Wood, J. Stanley, W. Otting | SUNPOWER ROBUST STIRLING CONVERTOR (SRSC) PROJECT OVERVIEW |
77 | C. G. Morrison | TEMPERATURE AND POWER SPECIFIC MASS SCALING FOR LEU CLOSED-CYCLE BRAYTON SYSTEMS FOR SPACE SURFACE POWER AND NUCLEAR ELECTRIC PROPULSION |
78 | K. Kazemzadeh, J. Mccoy | THE DEVELOPMENT, PROTOTYPING AND TESTING OF A SHOCK TOLERANT MILLI-WATT RADIOISOTOPE POWER SYSTEM |
79 | M. J. Eades, M. Reed, C. G. Morrison, W. Deason, S. Judd, V. Patel, P. Venneri | THE PYLON: COMMERCIAL LEU NUCLEAR FISSION POWER FOR LUNAR, MARTIAN, AND DEEP SPACE APPLICATIONS |
80 | R. C. O\\'Brien | THE SIRIUS-1 NUCLEAR THERMAL PROPULSION FUELS TRANSIENT TEST SERIES IN THE IDAHO NATIONAL LABORATORY TREAT REACTOR |
81 | D. Plachta, X. Wang, J. Hartwig | THERMAL MODEL OF A ZERO BOIL OFF SYSTEM FOR THE NUCLEAR THERMAL PROPULSION SYSTEM |
83 | X. Liu | THERMAL-HYDRAULIC DESIGN FEATURES OF A MICRO NUCLEAR REACTOR POWER SOURCE APPLIED FOR MULTI-PURPOSE |
84 | A. Aueron | TRADES ON DENSIFIED PROPELLANT FOR NUCLEAR THERMAL PROPULSION |
86 | J. J. Breedlove, T. M. Conboy, M. V. Zagarola | TURBO-BRAYTON CONVERTER FOR RADIOISOTOPE POWER SYSTEMS |
87 | M. F. Chaiken, M. A. Gibson | UPDATE ON RADIATION TESTING FOR SPACE FISSION POWER SYSTEMS |