Hypervelocity impact facility for simulating materials exposure to impact by space debris

Details Hypervelocity impact facility for simulating materials exposure to impact by space debris Hypervelocity impact facility for simulating materials exposure to impact by space debris

Jun 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992ldef.symp...39r&link_type=abstract

In NASA. Langley Research Center, Second LDEF Post-Retrieval Symposium Abstracts p 39 (SEE N92-27218 18-99)

Computer Science

Earth Orbital Environments, Environment Simulation, Hypervelocity Impact, Impact Damage, Particle Accelerators, Space Debris, Test Facilities, Long Duration Exposure Facility, Optical Materials, Paints, Protective Coatings, Solar Arrays

Scientific paper

The Space Power Institute at Auburn University has constructed an electromagnetically driven particle accelerator for simulating the effects of space debris on the materials for use in advanced spacecraft. The facility consists of a capacitively driven accelerator section, a drift tube and a specimen impact chamber. The drift tube is sufficiently long that all electrical activity has ceased prior to impact in the specimen chamber. The impact chamber is large enough to allow a wide range of specimen geometries, ranging from small coupons to active portions of advanced spacecraft. The electric drive for the accelerator consists of a 67 kJ, 50 k capacitor bank arranged in a low inductance configuration. The bank is discharged through an aluminum armature/plastic ablator plate/projectile load in roughly 1.2 microsec. The evaporation of the ablaitor plate produces an expanding gas slug, mostly H2, traveling at a velocity of some 60 km/sec. Because of the pressure and local density, the expanding gas cloud accelerates projectiles due to plasma drag. To date, we have utilized projectiles consisting of 100 micron SiC, 100 and 400 micron Al2O3, 100 and 145 micron olivines. Since many particles are accelerated in a given experiment, there is a range of velocities for each shot as well as some particle breakup. Advanced diagnostics techniques allow determination of impact coordinates, velocity, and approximate size for as many as 50 individual impacts in a given experiment. We routinely measure velocities in the range 1-15 km/sec. We have used this facility to study a variety of impact generated phenomena on coated surfaces, both paint and plastic, thermal blanket material, solar cell arrays, and optical materials such as glass and quartz lenses. The operating characteristics of the gun, the advanced diagnostic scheme, and the results of studies of crater morphology are described in detail. Projectile residue analysis, as a function of impact velocity for the materials listed above, is also discussed. Wherever possible, these results are compared to those obtained by LDEF investigators and future experiments suggested which could help to explain unique features associated with LDEF impacts.

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