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• 4 Airframe.
• The goals of the HSR Program require development of an advanced airframe structure that significantly outperforms conventional aluminum skin-stringer designs (i. ... In other words, the airframe structure typically weighs 25 percent of MTOW (maximum takeoff weight). ... In fact, the committee believes that the primary airframe structural design will have more impact on HSCT affordability than any other technological area. ...
• 4 Airframe This chapter discusses the process the HSR Program is using to select and develop candidate materials, to characterize and improve the service life of mate- rials in an HSCT environment, to identify and resolve manufacturing issues asso- ciated with new materials, to develop and validate low-weight structural designs, and to develop a feasible aerodynamic design that will enable the TCA to meet its weight and range goals. BACKGROUND The goals of the HSR Program require development of an advanced airframe structure that significantly outperforms conventional aluminum skin-stringer de- signs (i. ... In other words, the airframe structure typically weighs 25 percent of MTOW (maximum takeoff weight). ... In fact, the committee believes that the primary airframe structural design will have more impact on HSCT affordability than any other technological area. ...
• Except for the nose (radome) and leading edge structures on the wing and tail, the maximum effective skin temperatures estimated for the primary airframe structure on the fuselage, wing, and tail are 320°F. ... Two types of materials are generally available for airframe structures: com- posites, such as polymeric matrix composite (PMC) resin systems using carbon fibers; and metals. ... 4 critically affects development related to airframe materials, structures, and iPMCs suitable for high temperature airplane structure consist of high strength, high modulus car- bon fibers embedded in a high-temperature-resistant polymeric matrix (i. ...
• AIRFRAME Aluminum Titanium Epoxya BM'a Cyanatea Aryl-Ethera T. ... This is not the case with regard to airframe aerodynamics, the propul- sion system, or integrated aircraft systems. ...
• · finite element models of airframe structures · test data on wing and fuselage components The HSR Program will use these deliverables to evaluate the feasibility of meet- ing the weight and performance goals of the TCA and to support development of a refined aircraft configuration (the TCn). ...
• AIRFRAME 65 materials and to develop a fundamental understanding of high temperature mate- rial responses and degradation mechanisms. However, the HSR Program, with appropriate support from the airframe manufacturers and material suppliers, should also identify and develop critical enabling technologies to protect the vi- ability of developing a Mach 2. ...

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• Also contained in this section is information on the airframe and the major components. ...

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