By L.C. Chhabildas, Lee Davison, Y. Horie
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Extra info for High-pressure Shock Compression of SolidsI: The Science and Technology of High-velocity Impact
4. 5 kg mass. Nitrogen is presented as reference, and the 60 m launch tube is certainly a practical limiting value. Comparing the three gases, the highest muzzle velocity is obtained with hydrogen. The increase of the velocity between 6 m and 30 m is about 500 m/s for nitrogen, about 1500 m/s for helium, and about 2000 m/s for hydrogen. Between 30 m and 60 m, the increase of velocity is about 200 m/s for nitrogen, about 600 m/s for helium, and about 900 m/s for hydrogen. But the most important result of these calculations is that, with the same ﬁnal pressure, p0 , it is the lowest initial pressure (Case 1) that gives the highest velocity.
Hall, Chunk Projectile Launch Using the Sandia Hypervelocity Launcher Facility, Sandia National Laboratories Report No. SAND 94-1273 UC-410, Albuquerque, NM July 1994. 1 Light-Gas Gun Technology: A Historical Perspective 35 16. F. R. S. Army Armament Research and Development Command, Report No. ADOE-400 338, July 1979. 17. F. Lu and I. Marren Advanced Hypersonic Test Facilities, Vol. 198, pp. 531–554. A1AA Publication, New York City, 1995. 18. F. Swift, “Concept Deﬁnition Study for an Extremely Large Aerophysics Range Facility,” NASA Contractor Report 4491 NASA Langley Research Laboratories, Langley, VA.
Between 30 m and 60 m, the increase of velocity is about 200 m/s for nitrogen, about 600 m/s for helium, and about 900 m/s for hydrogen. But the most important result of these calculations is that, with the same ﬁnal pressure, p0 , it is the lowest initial pressure (Case 1) that gives the highest velocity. The reason for this is that the ﬁnal temperature is higher in the ﬁrst case than in the second case. 2 Scaling and Designing Large-Bore Two-Stage High Velocity Guns 43 Dynamic compression of the driving gas appears to be a good method for increasing the muzzle velocity.
High-pressure Shock Compression of SolidsI: The Science and Technology of High-velocity Impact by L.C. Chhabildas, Lee Davison, Y. Horie