An experimental study of the effect of the working fluid of a pneumatic launcher on the velocity of the projectile


Аuthors

Sinelnikov E. G.*, Zhitny M. V.**

Mlitary spaсe Aсademy named after A.F. Mozhaisky, St. Petersburg, Russia

*e-mail: vka@mil.ru
**e-mail: vka@mil.ru

Abstract

The paper presents an experimental study on the replacement of air with helium as the working fluid in a gas‑dynamic pulsed pneumatic launcher (developed at the A.F. Mozhaisky Military Space Academy) for laboratory simulation of particle impacts on spacecraft materials. The system enables testing at projectile velocities up to 1000 m/s. Velocity measurements were performed using an ACC 0022 “Strelets” frame chronograph, capable of measuring speeds up to 3000 m/s. To reduce measurement uncertainty caused by leading devices during subcaliber projectile tests, projectiles matching the barrel caliber were used. Functional velocity‑pressure relationships for both working fluids were derived via polynomial fitting using the least‑squares method. Experimental results show that helium significantly increases the initial projectile velocity compared to air under identical operating conditions. This confirms the technical advantage of helium for use in similar gas‑dynamic launch systems.

Keywords:

small-sized solid particle, high-speed impact, light-gas system, working fluid

References

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