Documents / Official release
This Defense Intelligence Reference Document, DIA-08-0912-008, is dated 12 January 2010. It was prepared by the Defense Warning Office's Acquisition Support Division at the Defense Intelligence Agency as one of a series of FY 2009 technology reports under the Advanced Aerospace Weapon System Applications program. It reviews materials for launch vehicles, space vehicles and reusable rocket engines, including aluminum alloys, polymer and metal matrix composites, titanium and nickel alloys, and titanium aluminides. It concludes that newer materials and integrated design could improve on the space shuttle.
From the source:Release of 2026-09-18 Incident: 1/12/10, Las Vegas, Nevada. Released with redactions. This document is a Defense Intelligence Reference Document (DIRD), a technical reference format used by the Defense Intelligence Agency (DIA) to capture baseline knowledge on a specific topic for later analytic use. DIRDs are best understood as reference and synthesis products rather than as original research. It is one of 38 DIRDs produced under the Advanced Aerospace Weapon System Applications Program (AAWSAP) between 2009 and 2011. Because AAWSAP’s scope permitted a broad range of supporting topics, not every DIRD in the series directly concerns aerospace systems or future threat assessment. The following summary reflects the DIRD’s scope and framing at the time of writing and should not be read as implying current validation of the concepts discussed. This DIRD surveys the structural materials needed for advanced aerospace platforms and argues that material choice cannot be separated from overall vehicle design, because launch vehicles, space vehicles, reusable systems, and propulsion hardware each face different temperature, durability, weight, and manufacturing constraints. The report reviews a range of candidate material classes, including advanced aluminum alloys; polymer-, aluminum-, and titanium-matrix composites; titanium alloys; nickel-base alloys; refractory metals; ceramic-matrix composites; carbon-carbon composites; and titanium aluminides. It emphasizes that balancing performance against practical limits such as fabrication methods, cost, inspection, contamination control, and service environment remains a major challenge. Its overall conclusion is that many promising materials exist, but their usefulness depends on application-specific tradeoffs and on closer integration of material selection with design and manufacturing, with some systems judged to be more valuable targets for development than others.
UNCLASSIFIED/ ,'FOR OFFl@IAL YSE OHL¥ • A couple of costly and highly visible TMC component test failures using TSM materials called into question the viability of TMCs. In truth, the real issue was one of quality and not the fundamental viability of the TMC material concept. • These failures led to extreme caution by the government, which promptly imposed stringent quality requirements on TSM. Consequently, TSM became a serious bottleneck for availability of TMCs with acceptable quality. As a result, numerous large, government-funded R&D programs fell behind schedule to the point that some were canceled and others were abandoned. • Other, less attractive SiC fibers were being developed during this period, including Nicalon in Japan and Sigma in the United Kingdom. Because SiC fiber and TMCs were deemed strategic materials and neither of these alternate fibers was produced in the United States, there was reluctance to experiment with them, and the U.S. government occasionally prohibited their use in federally funded R&D programs. • The issue of fiber availability became a major distraction from the real business at hand-that is, improving the consistency and reducing the cost of the TMC product. • In the end, TSM partially relented, but by then such limited interest in TMCs existed that the original opportunity was lost. Furthermore, there still was no concrete evidence that TMCs could be produced with sufficiently consistent properties that they could be considered an engineering material (at any cost). • In the mid-1990s, a cost study that assumed fiber availability showed that TMCs that meet specification properties could be manufactured for about $500/lb (in 1995 $) if the use volume was about 10,000 lb/year. Finding enough low-risk, high-value applications to consume this quantity of TMCs was not deemed possible. • Consequently, work on TMCs halted after an investment of about $500 million of U.S. government funds and a (presumably) comparable, but less well known private sector (mostly independent R&D $) investment. • One lesson from this is that a credible market and cost study should be undertaken before embarking on a major R&D program to develop revolutionary materials such as TMCs. The foregoing discussion exemplifies the challenges associated with developing and commercializing a revolutionary new materials system. New material concepts originating from nonproduction sources such as national laboratories or research universities should be approached with caution and never be put on the critical path of product design. Even if a new material is vetted through an established production source, the timing of full commercialization should be carefully examined. Ni-base Alloys Ni-base alloys have been considered real engineering materials for at least 40 years. Because of their relatively low rate of strength loss with increasing temperature, Ni base alloys are also called "superalloys." They are commonly used at temperatures well in excess of half of their melting point (Tm), which is the accepted useful limit for most structural metallic materials. There is no other class of structural alloys for which this is true. Ni-base alloys have been used in turbine engines of all types almost since their 16 UNCLASSIFIED/ /FOA OFFICiIAk Wlilii 0PU.¥
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Official release, from the pursue collection. The PDF is mirrored here; the original link is above. 27 pages are in the text index: search them above, or from the library's search.