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Pressure correction of ultrasonic regression rate measurements of a hybrid slab motor AIAA-99-2319

Pressure correction of ultrasonic regression rate measurements of a hybrid slab motor AIAA-99-2319
Paper規格・テクニカルリポート類
Serin, Nadir, Chiaverini, Martin J, Harting, George C, Kuo, Kenneth K1999<M-AIAA-99-2319>
National Diet Library

Marus ISRU CO/O2 hybrid engine development status AIAA-2000-1066

Marus ISRU CO/O2 hybrid engine development status AIAA-2000-1066
Paper規格・テクニカルリポート類
Rice, Eric E, Chiaverini, Martin J, St. Clair, Christopher P, Knuth, William H.; Gustafson, Robert J2000<M-AIAA-2000-1066>
National Diet Library

Solid-fuel regression rate and combustion behavior of vortex hybrid rocket engines AIAA-99-2318

Solid-fuel regression rate and combustion behavior of vortex hybrid rocket engines AIAA-99-2318
Paper規格・テクニカルリポート類
Knuth, William H, Chiaverini, Martin J, Gramer, Daniel J, Sauer, J. Arthur1999<M-AIAA-99-2318>
National Diet Library

Regression rate and heat transfer correlations for HTPB/GOX combustion in a hybrid rocket motor AIAA-98-3185

Regression rate and heat transfer correlations for HTPB/GOX combustion in a hybrid rocket motor AIAA-98-3185
Paper規格・テクニカルリポート類
Chiaverini, Martin J, Kuo, Kenneth K, Peretz, Arie, Harting, George C1998<M-AIAA-98-3185>
National Diet Library

Development and testing of a vortex-driven, high-regression rate hybrid rocket engine AIAA-98-3507

Development and testing of a vortex-driven, high-regression rate hybrid rocket engine AIAA-98-3507
Paper規格・テクニカルリポート類
Knuth, William H, Gramer, Daniel J, Chiaverini, Martin J, Sauer, J. Arthur1998<M-AIAA-98-3507>
National Diet Library

Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine AIAA-98-3348

Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine AIAA-98-3348
Paper規格・テクニカルリポート類
Knuth, William H, Chiaverini, Martin J, Gramer, Daniel J, Sauer, J. Arthur1998<M-AIAA-98-3348>
National Diet Library

Preliminary CFD analysis of the vortex hybrid rocket chamber and nozzle flow field AIAA-98-3351

Preliminary CFD analysis of the vortex hybrid rocket chamber and nozzle flow field AIAA-98-3351
Paper規格・テクニカルリポート類
Knuth, William H, Gramer, Daniel J, Chiaverini, Martin J, Sauer, J. Arthur, Whitesands, R. Harold, Dill, Richard A1998<M-AIAA-98-3351>
National Diet Library

Heat flux and internal ballistic characterization of a hybrid rocket motor analog AIAA-97-3080

Heat flux and internal ballistic characterization of a hybrid rocket motor analog AIAA-97-3080
Paper規格・テクニカルリポート類
Chiaverini, Martin J, Kuo, Kenneth K, Peretz, Arie, Harting, George C1997<M-AIAA-97-3080>
National Diet Library

Combustion of solid fuel slabs with gaseous oxygen in a hybrid motor analog [microform] / Martin J. Chiaverini ... [et al.] ([NASA contractor report] ; NASA-CR-201116)

Combustion of solid fuel slabs with gaseous oxygen in a hybrid motor analog [microform] / Martin J. Chiaverini ... [et al.] ([NASA contractor report] ; NASA-CR-201116)
Microform図書
1995<YCA-NAS 1.26:201116>
National Diet Library

Fuel decomposition and boundary-layer combustion processes of hybrid rocket motors AIAA-95-2686

Fuel decomposition and boundary-layer combustion processes of hybrid rocket motors AIAA-95-2686
Paper規格・テクニカルリポート類
Chiaverini, Martin J, Harting, George C, Lu, Yeu-Cherng, Kuo, Kenneth K, Serin, Nadir, Johnson, David K1995<M-AIAA-95-2686>
National Diet Library

Fundamentals of hybrid rocket combustion and propulsion

Fundamentals of hybrid rocket combustion and propulsion
Paper図書
edited by Martin J. Chiaverini, Kenneth K. KuoAmerican Institute of Aeronautics and Astronauticsc2007
Other Libraries in Japan
  • Author HeadingChiaverini, Martin J. Kuo, Kenneth K.

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