Browse Topic: Protective clothing
ABSTRACT Previous efforts demonstrated the ability to achieve a 30% weight reduction for a MIL-DTL-27422D Phase I test cube construction with Protection Level A gunfire performance, using a lightweight 2-ply exoskeleton design to replace the 4-ply construction otherwise required to meet crash impact test requirements. An additional 20% reduction in weight was projected by replacing the natural gum rubber (NGR) used in conventional fuel bladder constructions with a lightweight formulation. This paper reviews the technical efforts executed to support the transition of the lightweight exoskeleton construction to the Apache AH-64 helicopter. The fuel bladders made with the lightweight sealant were 15.5% lighter for the AH-64 FWD fuel bladder and 13.2% lighter for the AFT. Additional weight savings based on the 2-ply exoskeleton construction was not realized as the existing AH-64 fuel bladders are already relatively lightweight constructions. The final AH-64 fuel bladders demonstrated the ability to be qualified to all MIL-DTL-27422E performance requirements; however, the program concluded without demonstrating Protection Level A gunfire performance. Importantly, there did not appear to be any discernable difference in the self-sealing performance of the fuel bladders made with the lightweight sealant and the constructions based on conventional NGR sealant. While additional work may be required to address this performance deficiency, there were several issues that were noted during the Phase II gunfire testing that should be reviewed and resolved prior to additional testing.
Metering structures of remote sensing instruments often have large openings or access holes. Shear panels that are X-shaped, such as those proposed for the Neutron Star Interior Composition Explorer (NICER), generally consist of C-channels and L-brackets to minimize structural distortion. This type of metering structure has large openings on the sides. Structural panels that have large access holes, such as those studied for the Landsat Operational Land Imager (OLI), generally consist of aluminum honeycomb panels with composite facesheets. Both types of metering structure require multilayer insulation (MLI) blankets to shield the internal components such as optics from sunlight and Earth albedo, and to minimize heat loss to 3K space by radiation. The issues of conventional MLI blankets for these metering structures include MLI sagging, stray light, and risk of micrometeoroid damage to optics.
Currently, lead and lead-based materials are used to fabricate shields not only for X-rays, but also for other types of radiation. With the growing environmental concern about the toxicity of lead, and the high costs associated with transporting heavy lead-based shields in spacecraft, alternatives are needed for fabricating X-ray shields that are less toxic and lighter.
ABSTRACT One of the most famous of Augustine's Laws involved the ever-escalating costs of aircraft over time. Law Number XVI states, "In the year 2054, the entire defense budget will purchase just one aircraft. This aircraft will have to be shared by the Air Force and Navy 3- 1/2 days each per week except for leap year, when it will be made available to the Marines for the extra day." This particular reference involved tactical aircraft but the same trend can be observed for other types of military hardware. This paper addresses and attempts to explain this phenomenon as it applies to the rotorcraft industry. For example, increasing demand for more survivable rotorcraft, and more survivable payloads that must be carried by rotorcraft (eg., HMMWVs, soldier body armor, etc.), result in not only higher unit costs but in higher mission costs.
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