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AAWSAP DIRD, Metallic Glasses for Aerospace Applications, December 2009

U.S. Department of War · 2009-12-14 · 30 pages · text from the file's own layer

This Defense Intelligence Reference Document, dated 14 December 2009, was prepared by the Defense Intelligence Agency's Defense Warning Office under its Advanced Aerospace Weapon System Applications program. It is a technical review of metallic glasses that covers their structure, processing, mechanical behavior and possible aerospace uses. It concludes that composites with ductile dendrites in a glass matrix hold the most promise for structural use. It also finds that widespread aerospace adoption depends on developing new lightweight glass-forming alloys.

From the source:Release of 2026-09-18 Incident: 12/14/09, 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 metallic glasses as a potentially important class of aerospace materials and describes their amorphous structure as offering very high strength and unusual manufacturing advantages, but also significant drawbacks, especially poor ductility and fatigue resistance. The document concludes that the most promising aerospace applications are likely to come from metallic-glass-matrix composites rather than single-phase glasses, because these composites can retain high strength while greatly improving fracture toughness and fatigue performance, potentially enough to substitute for high-strength steels in some space-limited structural uses. At the same time, the report judges that broader aerospace use will depend on substantial progress over the next 20–50 years in alloy design, processing, and especially the development of lightweight systems, including aluminum-based options.

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Metallic glass foams (see above) also provide intriguing possibilities for structural
applications. It has recently been shown that metallic glass foams with outstanding
strength can be formed by controlling the size of the ligaments between pores. 40 This is
a new development, and these foams have not been fully characterized, but it seems
likely that optimized foams will have a specific stiffness (E/p) superior to that of
polymer foams, along with high strength and acoustic damping. Such structural foams
could be useful in applications requiring strength and stiffness under compressive loads,
such as structural panels for extraterrestrial buildings. Conceivably, such structural
foams might even be produced on site (from raw feedstock), reducing the volume of
material that needs to be launched.
A final possibility is that metallic glasses might be combined with polymer composites
into metal-fiber laminate materials. Similar laminates (with crystalline aluminum alloys)
are being employed in large quantities on the new Airbus 380 and are likely to find
increased application in the future. 4 1 The use of metallic glasses in these laminates is
appealing because of their high specific strength (although the specific stiffness is lower
than that of aluminum). Furthermore, the individual layers in the laminate are
sufficiently thin that a wide range of glass-forming alloys might be considered (in
contrast to thicker structural sections, which will be limited by the glass-forming ability
of the alloy).
OTHER APPLICATIONS
Monolithic metallic glasses are unique among metallic materials in having no
microstructure at length scales of more than a few atomic spacings. In principle then,
metallic glasses should be capable of replicating features down to this scale. This
possibility is facilitated by the ability of metallic glasses to be formed in the supercooled
liquid temperature range with controllable viscosity . Indeed, superplastic forming of
metallic glass surfaces with features as small as 13 nanometers has been
demonstrated. 42 This ability could be exploited for direct embossing of nanostructures
in polymers or other materials. Structures on this length scale are also potentially
useful as diffraction gratings for ultraviolet and so~ x-ray radiation.
In a related area, metallic glasses have a variety of useful properties for application in
micro-electromechanical system (MEMS) actuators, including large elastic strains and
high resilience (elastic strain energy storage), good corrosion and wear resistance, and
an excellent surface finish. 43 The scale of these devices is smaller than the plastic zone
size (Equation 1 above), making brittle fracture unlikely. Furthermore, a much wider
variety of amorphous alloys can be made in thin film form (by vapor deposition) than is
possible by casting.
Finally, the magnetic properties of certain amorphous alloys have long been exploited.
For instance, their low coercivity and high electrical resistivity make ferromagnetic
amorphous alloys attractive as high-efficiency electrical transformers, particularly at
high frequencies. Such applications are likely to continue well into the future.
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Official release, from the pursue collection. The PDF is mirrored here; the original link is above. 30 pages are in the text index: search them above, or from the library's search.