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filament-wound struts
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Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003476
EISBN: 978-1-62708-195-5
... shows a PMR-15 sandwich structure for which the skins were procured and then bonded to a glass-polyimide honeycomb using a commercially available adhesive based on PMR- 15 ( Ref 26 ). Interest has also been shown in applying PMR-15 composites to filament-wound structures. In 1985, a small, integrally...
Abstract
High-temperature-resistant polymers are used in aerospace, electronic, and other applications that demand outstanding elevated-temperature physical and mechanical properties. This article discusses the general characteristics of condensation-type polyimides and polymerization of monomer reactants (PMR) polyimides. It provides information on the applications of PMR-15 with illustrations.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003475
EISBN: 978-1-62708-195-5
...; low-modulus carbon-carbon thermal doublers; K13C2U/PC for battery support and radiator H/C, honeycomb; PC, polycyanate Rocket motor cases manufactured with filament-wound composites since the 1950s Table 5 Rocket motor cases manufactured with filament-wound composites since the 1950s...
Abstract
This article discusses composites for unmanned space vehicles and provides an overview of key design drivers, challenges, and environment for use of composites in spacecraft, launch vehicles, and missiles. It describes the design allowable properties of composite materials. The article provides information on the specific state-of-the-art applications of composite materials for spacecraft missiles and launch vehicles. A discussion on the key applications, including solid rocket motor casings, payload fairings, and payload support structures, is presented.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003361
EISBN: 978-1-62708-195-5
... curvatures) than filament-wound preforms. The interlaced nature of braids also provides a higher level of structural integrity, which is essential for ease of handling, joining, and damage resistance. While it is easier to provide hoop (90°) reinforcement by filament winding, longitudinal (0°) reinforcement...
Abstract
Braided structures are unique in their high level of conformability, torsional stability, and damage resistance. This article describes the classifications of braiding such as two-dimensional braiding and three-dimensional braiding. It presents the governing equations for computer-controlled braiding in a table. The article lists the applications of braided fabrics and composites. It discusses the formation, structure, and properties of two-dimensional braid composites and three-dimensional braid composites: the damage tolerance and the impact damage limitation.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003477
EISBN: 978-1-62708-195-5
.... The predominant fiber used in interior composites is fiberglass; however, carbon fiber use is increasing as structural applications increase. For example, a filament-wound door spring is employed on the 767. Using unidirectional carbon fibers in an epoxy matrix, the springs are only one-third as heavy...
Abstract
This article provides information on the applications of fiber-reinforced composites in commercial and military aircrafts. It tabulates the composite components in various types of aircraft. The applications of the composites in the components of Boeing 727, 737, 757, 767, 777, and 777-200 are schematically illustrated.
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.9781627081627
EISBN: 978-1-62708-162-7
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.9781627081993
EISBN: 978-1-62708-199-3