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Scaling numerical models for hypervelocity test sled slipper-rail impacts
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Hypervelocity Gouging Impacts (Progress In Astronautics And Aeronautics)
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Hypervelocity impact. The proceedings are published in three volumes. Nine papers were selected for presentation and publication in the Classified Proceedings, and eight papers were selected for presentation and publication in the NOFORN Proceedings. The cell's outer construction was a 24 mil-thick Inconel pressure vessel. A sheet of 1. The hypervelocity gun used was a 7. The battery cells were electrically charged to about 75 percent of capacity, then back-filled with hydrogen gas to psi simulating the full charge condition. Impacts in the dome area top and the electrode area middle of the battery cells were investigated.
Five tests on battery cells were performed.
Sliding Instabilities and Hypervelocity Gouging - IEEE Journals & Magazine
The results revealed that in all of the test conditions investigated, the battery cells simply vented their hydrogen gas and some electrolyte, but did not burst or generate any large debris fragments. The majority of the specimens tested consists of a foil gauge exterior honeycomb panel, composed of either Inconel or Ti-6Al-4V, backed with 2.
Other tested specimens include titanium multi-wall sandwich coupons as well as TPS using a second honeycomb sandwich in place of the foil backing. An improved test fixture was designed and fabricated to hold specimens firmly in place during impact. Projectile diameter, honeycomb sandwich material, honeycomb sandwich facesheet thickness, and honeycomb core cell size were examined to determine the influence of TPS configuration on the level of protection provided to the substructure crew, cabin, fuel tank, etc.
Pictures and descriptions of the damage to each specimen are included. Hypervelocity impact physics. All large spacecraft are susceptible to impacts by meteoroids and orbiting space debris. These impacts occur at extremely high speed and can damage flight-critical systems, which can in turn lead to a catastrophic failure of the spacecraft.
Therefore, the design of a spacecraft for a long-duration mission must take into account the possibility of such impacts and their effects on the spacecraft structure and on all of its exposed subsystems components. Hypervelocity impact mechanics was used to analyze the damage that occurs when a space vehicle is impacted by a micrometeoroid or a space debris particle. An impact analysis of over test specimens was performed to generate by a hypervelocity impact damage database. Hypervelocity Impact Test Facility: A gun for hire.
Johnson, Calvin R. An affordable technique has been developed to duplicate the types of impacts observed on spacecraft, including the Shuttle, by use of a certified Hypervelocity Impact Facility HIF which propels particulates using capacitor driven electric gun techniques. The fully operational facility provides a flux of particles in the micron diameter range with a velocity distribution covering the space debris and interplanetary dust particle environment. HIF measurements of particle size, composition, impact angle and velocity distribution indicate that such parameters can be controlled in a specified, tailored test designed for or by the user.
Unique diagnostics enable researchers to fully describe the impact for evaluating the 'targets' under full power or load. Users regularly evaluate space hardware, including solar cells, coatings, and materials, exposing selected portions of space-qualified items to a wide range of impact events and environmental conditions.
Benefits include corroboration of data obtained from impact events, flight simulation of designs, accelerated aging of systems, and development of manufacturing techniques. At Auburn, the solar cells and array blanket materials received several hundred impacts from particles in the micron to micron range with velocities typically ranging from 4.
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