| Starting transient of solid-propellant ocket motors with high internal gas velocities A Peretz, KK Kuo, LH Caveny, M Summerfield AIAA Journal 11 (12), 1719-1727, 1973 | 118 | 1973 |
| Radiative ignition of double-base propellants. I-Some formulation effects L DeLuca, LH Caveny, TJ Ohlemiller, M Summerfield Aiaa Journal 14 (7), 940-946, 1976 | 102 | 1976 |
| Agglomeration and ignition mechanism of aluminum particles in solid propellants A Gany, LH Caveny Symposium (International) on Combustion 17 (1), 1453-1461, 1979 | 85 | 1979 |
| Radiative ignition of double base propellants. II-Pre-ignition events and source effects L DeLuca, TJ Ohlemiller, LH Caveny, M Summerfield Aiaa Journal 14 (8), 1111-1117, 1976 | 84 | 1976 |
| Solid rocket enabling technologies and milestones in the United States LH Caveny, RL Geisler, RA Ellis, TL Moore Journal of propulsion and power 19 (6), 1038-1066, 2003 | 65 | 2003 |
| The mechanism of super-rate burning of catalyzed double base propellants N Kubota, TJ Ohlemiller, LH Caveny, M Summerfield Symposium (International) on Combustion 15 (1), 529-537, 1975 | 65 | 1975 |
| Nitramine flame chemistry and deflagration interpreted in terms of a flame model M Ben-Reuven, LH Caveny AIAA Journal 19 (10), 1276-1285, 1981 | 63 | 1981 |
| Site and mode of action of platonizers in double base propellants N Kubota, TJ Ohlemiller, LH Caveny, M Summerfield AIAA Journal 12 (12), 1709-1714, 1974 | 56 | 1974 |
| Theory of dynamic extinguishment of solid propellants with special reference to nonsteady heat feedback law M Summerfield, LH Caveny, RA Battista, N Kubota, YA Gostintsev, ... Journal of Spacecraft and Rockets 8 (3), 251-258, 1971 | 52 | 1971 |
| Influence of embedded metal fibers on solid-propellant burning rate. LH Caveny, RL Glick Journal of Spacecraft and Rockets 4 (1), 79-85, 1967 | 52 | 1967 |
| Aluminized solid propellants burning in a rocket motor flowfield A Gany, LH Caveny, M Summerfield AIAA Journal 16 (7), 736-739, 1978 | 50 | 1978 |
| Breakup of Al/Al2O3 agglomerates in accelerating flowfields LH Caveny, A Gany AIAA Journal 17 (12), 1368-1371, 1979 | 47 | 1979 |
| Dynamic effects on ignitability limits of solidpropellants subjected to radiative heating TJ Ohlemiller, LH Caveny, L DeLuca, M Summerfield Symposium (International) on Combustion 14 (1), 1297-1307, 1973 | 45 | 1973 |
| Thrust and ignition transients of the Space Shuttle solid rocket motor LH Caveny, KK Kuo, BW Shackelford Journal of Spacecraft and Rockets 17 (6), 489-494, 1980 | 38 | 1980 |
| Orbit-raising and maneuvering propulsion: research status and needs LH Caveny American Institute of Aeronautics and Astronautics, 1984 | 30 | 1984 |
| Flame zone and sub-surface reaction model for deflagrating RDX M BenReuven, LH Caveny, RJ Vichnevetsky, M Summerfield Symposium (International) on Combustion 16 (1), 1223-1233, 1977 | 29 | 1977 |
| Solid propellant ignition and other unsteady combustion phenomena induced by radiation L De Luca, TJ Ohlemiller, LH Caveny, M Summerfield Aerospace and Mechanical Sciences Department, Princeton University …, 1976 | 25 | 1976 |
| Restart transients of hybrid rocket engines. MA Saraniero, LH Caveny, M Summerfield Journal of Spacecraft and Rockets 10 (3), 215-217, 1973 | 23 | 1973 |
| Ignition transients of large segmented solid rocket boosters LH Caveny, KK Kuo NASA, 1976 | 22 | 1976 |
| Influence of thermal radiation on solid propellant burning rate LH Caveny, TJ Ohlemiller, M Summerfield AIAA Journal 13 (2), 202-205, 1975 | 22 | 1975 |