Defense Intelligence Reference Document Materials For Advanced Aerospace Platforms

Defense Intelligence Agency · 27 pages · text from the file's own layer

This Defense Intelligence Reference Document from the Defense Intelligence Agency, dated 12 January 2010, is one of a series of advanced technology reports produced in FY 2009 under the Advanced Aerospace Weapon System Applications (AAWSA) 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, ceramics and titanium aluminides. It concludes that newer materials and design methods offer many ways to improve structural efficiency and cost compared with the space shuttle.

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“The Times”14 pages

p. 4 …time consideration of materials capability. This approach led to significant compromises at later stages in the…
p. 8 …An additional issue is out time-the time the pre-preg can be out of the…
p. 9 …Clearly, the time required for layup places practical limitations on component size. • In automated tow placement…
p. 11 …The TOS, like any chemical reaction, is determined by both time and temperature. The glass transition…
p. 12 …The choice of Ti-10-2-3 for the landing gear truck beam reflects the time…
p. 14 …Earlier programs such as the DynaSoar reusable reentry glider devoted considerable time and resources to examining…
p. 15 …mission requirements, including the number of missions and expectations for turnaround time between missions. Furthermore, operational…
p. 16 …the thermal soakback from the hot external structure can lead to softening in real time or…
p. 17 …If an adequate market for AMCs were to emerge, the time and cost to make them…
p. 21 …Even if a new material is vetted through an established production source, the timing of full…
p. 24 …times that of the unreinforced matrix. Clearly, the nature of the fiber- matrix interface determines the…
p. 25 UNCLASSIFIED11,ff8"1 IPPl9ML lt91!! OIIEI Therefore, instabilities that cause time-dependent reductions in toughness must…
p. 26 …cracking would greatly reduce the intermission refurbishment time and cost. Traditionally, the cryopump rotating parts have…
p. 27 …The issue of long lead time holding back these improved design methods is most often one…

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Figure 4 shows an example of a TI matrix composite (TMC) cross section.
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Figure 4. Cross-Section Micrograph of a Ti Matrix Composite. Small, dark centers
of fibers are C monofilament substrates for deposition of SiC (light micrograph).
Material system: Matrix alloy - Ti-6242; Fiber - SiC about 5.6-mil-diameter SCS-6
Table 2 shows that the strength and stiffness properties of TMCs can exceed those of
the Ti matrix (or other a+/3 Ti alloys) by more than a factor of two with no increase in
density. So why are TMCs not in widespread use? The foremost reason is cost. Another
reason is the availability of SiC fiber for TM Cs.
• During the 1990s, when the U.S. government (mainly DoD) was interested in and
provided development money for TMC R&D, the most attractive reinforcing fiber was
SCS-6Tr,1, which was produced exclusively by Textron Specialty Materials (TSM) in
Lowell, MA.
• Unfortunately (at least in hindsight), TSM made a business decision not to sell fiber
and to instead forward-integrate and sell TMC components or finished TMC mill
products. This decision stemmed in part from TSM's negative business experience
with development of B-based fiber (Boro-SiC™) for first-generation TMCs.
• Prior to making this business decision, TSM did not develop sufficient TMC-
manufacturing expertise to properly position itself as a producer of TMC products
with consistent properties.
15
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Report, from the dia collection. The PDF is mirrored here; the original link is under it. 27 pages are in the text index: search them above, or from the library's search.