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Rocket nozzles

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Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000117
EISBN: 978-1-62708-313-3
...) Haynes 242 Seal rings, duct segments, casings, fasteners, rocket nozzles, and pumps High strength, fatigue resistance, and oxidation resistance up to 760 °C (1400 °F), relatively low CTE Haynes HR-120 Heat treating fixtures and industrial heating applications as an alternative to IN-800H...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2008
DOI: 10.31399/asm.tb.emea.t52240583
EISBN: 978-1-62708-251-8
... industry because it resists the corrosive effects of molten zinc. It has also proved effective in rocket nozzles and has the potential of offering enhanced performance in applications where any erosive effects are a factor. The importance of molybdenum-rhenium alloys is due to the “rhenium effect,” which...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2011
DOI: 10.31399/asm.tb.cfw.t52860115
EISBN: 978-1-62708-338-6
...) Fig. 9.28 Pressure vessel burst test examples. (a) 92 in. (2336 mm) large aramid-fiber/epoxy space motor case burst. (b) S-glass pressure vessel burst. (c) Tactical rocket motor carbon-fiber/epoxy burst from high-speed film. (d) Carbon-fiber/epoxy space motor pressure vessel burst on high-speed film...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550569
EISBN: 978-1-62708-307-2
... for rocket engines . Integrally bladed disks (“blisks”) for rocket engine turbopumps have been produced from carbon-fiber-reinforced SiC. Figure 11.16 shows the Fastrac engine developed by the National Aeronautics and Space Administration (NASA) and the locations of the turbopump and blisk. The blisks were...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.tb.hpcspa.t54460067
EISBN: 978-1-62708-285-3
... properties. On the other hand, the particle velocity and temperature, v p and T p , can be regarded as impact conditions that depend mainly on the process parameters, such as gas temperature, gas pressure, and nozzle dimensions. There is also an influence of the particle temperature on the critical...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2013
DOI: 10.31399/asm.tb.mfub.t53740325
EISBN: 978-1-62708-308-9
... products include crucibles, rocket nozzles, and other high-temperature components, linings for chemical vessels, and coatings for electronic components. These refractory metals are deposited at temperatures far below their melting points or sintering temperatures, and coatings can be produced...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060231
EISBN: 978-1-62708-343-0
... of the Space Shuttle Main Engine (SSME). As general background, the Space Shuttle of the United States ( Fig. 10.1 ) was the world’s first reusable STS. The launch occurs from two types of rockets: a pair of solid-fueled boosters bolted to the sides of the prominent central liquid fuel tank, and a cluster...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000001
EISBN: 978-1-62708-313-3
... of relatively high mechanical strength and surface stability at high temperature ( Ref 1 ). The primary application that has driven superalloy development is for use as air foils in the hot section of gas turbine engines (GTEs), but they have been used successfully in other applications, such as rocket...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870573
EISBN: 978-1-62708-314-0
...-temperature applications, C-C composites offer exceptional thermal stability greater than 4000 °F (2205 °C) in nonoxidizing atmospheres along with low densities of 0.054 to 0.072 lb/in. 3 (1.49 to 1.99 g/cm 3 ). Carbon-carbon composites are used in rocket nozzles, nose cones for reentry vehicles, leading...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2011
DOI: 10.31399/asm.tb.cfw.9781627083386
EISBN: 978-1-62708-338-6
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2001
DOI: 10.31399/asm.tb.secwr.t68350125
EISBN: 978-1-62708-315-7
... been developed for specific uses, including wear resistance, chemical resistance, high reflectivity, electrical resistance, and prevention of hydrogen diffusion. Ceramic-coated metals are used for furnace components, heat treating equipment, chemical processing equipment, heat exchangers, rocket motor...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120085
EISBN: 978-1-62708-269-3
... for planishing are held to a minimum by placing the blast nozzle at a distance of approximately 50 mm (2 in.) from the workpiece and by using an angle of impingement of 60°. Rocket motor-case assemblies have been dry blasted after final stress relieving at 480 to 540 °C (895–1005 °F). Blasting...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550457
EISBN: 978-1-62708-307-2
... in the aerospace and defense sectors of the market. In one example, a rocket motor shell was produced by filament winding of SCS-6 fibers and plasma spraying with an aluminum alloy. The rocket motor was reported to have been successfully fired and to have withstood the extreme temperatures, pressures...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.cfap.t69780115
EISBN: 978-1-62708-281-5
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870401
EISBN: 978-1-62708-314-0
... composites are used for ablative exhaust nozzles for rockets and as a starting material in the production of carbon-carbon composites. They basically encapsulate themselves in char and therefore do not produce much smoke. The principal volatile decomposition products are methane, acetone, carbon monoxide...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.horfi.t51180029
EISBN: 978-1-62708-256-3
... around component testing and test areas and you will learn that all potential causes of failures or events are taken seriously, no matter how ridiculous they may seem. I was working in a company that produced rocket engines. Part of that business consisted of regularly performing rocket engine tests. One...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2015
DOI: 10.31399/asm.tb.tpmpa.t54480265
EISBN: 978-1-62708-318-8
... in.) Welding speed, mm/min (in./min) 500 (20) 380 (15) Arc current, A 185 190 Arc voltage, V 21 26 Gas flow rate, cm 3 /h × 10 4 (ft 3 /h)  Nozzle 23 (8) 34 (12)  Shielding 34 (12) 130 (45) (a) Electrode set back 3.2 mm (⅛ in.) from face of torch nozzle, with nozzle-to-work...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870085
EISBN: 978-1-62708-299-0
..., specimens have been attached to rocket sleds propelled at speeds up to 1700 m/s (5580 ft/s) through an artificial rain field. Wind tunnels have also been adapted for rain erosion tests. As noted earlier, cavitation erosion test methods such as the vibratory method ( Fig. 6 ) have also been used...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550193
EISBN: 978-1-62708-307-2
... grinding has largely replaced attritioning and ball milling as the major powder production technique. In the impact-grinding process, shown in Fig. 4.3 , coarse powder is fed from the feed hopper into a gas stream. As the gasborne powder is carried through a nozzle, it accelerates and impacts...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550001
EISBN: 978-1-62708-307-2