This paper reports a theoretical and numerical study aimed at increasing the operating efficiency of two-stage light-gas guns by appropriately changing their working conditions. In particular, a method is presented for increasing the projectile speed without any rise of the maximum breech pressure. The classic design theory of two-stage guns starts from the assumption that the highest velocity is reached in a gun which constantly maintains the maximum acceptable pressure at the base of the projectile during the full launching time. The main drawback of this working condition is that it may require an unfeasible rise of the gun maximum pressure, especially when very high muzzle speed is requested. To overcome this limitation, a new reference...
A gasdynamic gun driven by gaseous detonation was developed to address the disadvantages of the insu...
This paper reports development of a new trigger system for a high speed gas gun and experimental res...
AbstractA traditional difficulty with high-explosive hypervelocity launching techniques is that extr...
A two-stage light gas gun driven by gaseous detonation was newly constructed, which can make up for ...
Abstract A preliminary version of Two Stage Light Gas Gun for impact testing directly derived from f...
Space debris poses a major risk to spacecraft. In low earth orbit, impact velocities can be 10 11 km...
We report a study in the field of gun design and optimization, paying particular attention to the is...
A new gasdynamic launcher is described, in which intact projectiles weighing at least 1 gram can be ...
This paper discusses ballistic range testing at muzzle velocities of 0.7 to 2.7 km/s. Herein, we rev...
A new gasdynamic launcher is described, in which intact projectiles weighing at least one gram can b...
Hypervelocity impact experiments that reproduce on-orbit collisions between micrometeoroids or orbit...
The performance of UBC two-stage light-gas gun and the associated diagnostics systems were examined ...
The Joint Actinide Shock Physics Experimental Facility (JASPER) located in area 27 at the Nevada Tes...
A comparison of techniques for obtaining projectile velocity history on a two-stage launcher and dis...
A new two-stage light-gas gun type accelerator was developed at Fraunhofer EMI. The pumping stage is...
A gasdynamic gun driven by gaseous detonation was developed to address the disadvantages of the insu...
This paper reports development of a new trigger system for a high speed gas gun and experimental res...
AbstractA traditional difficulty with high-explosive hypervelocity launching techniques is that extr...
A two-stage light gas gun driven by gaseous detonation was newly constructed, which can make up for ...
Abstract A preliminary version of Two Stage Light Gas Gun for impact testing directly derived from f...
Space debris poses a major risk to spacecraft. In low earth orbit, impact velocities can be 10 11 km...
We report a study in the field of gun design and optimization, paying particular attention to the is...
A new gasdynamic launcher is described, in which intact projectiles weighing at least 1 gram can be ...
This paper discusses ballistic range testing at muzzle velocities of 0.7 to 2.7 km/s. Herein, we rev...
A new gasdynamic launcher is described, in which intact projectiles weighing at least one gram can b...
Hypervelocity impact experiments that reproduce on-orbit collisions between micrometeoroids or orbit...
The performance of UBC two-stage light-gas gun and the associated diagnostics systems were examined ...
The Joint Actinide Shock Physics Experimental Facility (JASPER) located in area 27 at the Nevada Tes...
A comparison of techniques for obtaining projectile velocity history on a two-stage launcher and dis...
A new two-stage light-gas gun type accelerator was developed at Fraunhofer EMI. The pumping stage is...
A gasdynamic gun driven by gaseous detonation was developed to address the disadvantages of the insu...
This paper reports development of a new trigger system for a high speed gas gun and experimental res...
AbstractA traditional difficulty with high-explosive hypervelocity launching techniques is that extr...