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Structural Stiffness And Free Play Analysis Of The Space Shuttle Solid Rocket Booster Field Joint
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Book Synopsis Structural Stiffness and Free-play Analysis of the Space Shuttle Solid Rocket Booster Field Joint by : Dan Allen Bodeker
Download or read book Structural Stiffness and Free-play Analysis of the Space Shuttle Solid Rocket Booster Field Joint written by Dan Allen Bodeker and published by . This book was released on 1999 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722779245 Total Pages :54 pages Book Rating :4.7/5 (792 download)
Book Synopsis Structural Stiffness Characteristics of the Solid Rocket Booster Field Joint by : National Aeronautics and Space Administration (NASA)
Download or read book Structural Stiffness Characteristics of the Solid Rocket Booster Field Joint written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-16 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Space Shuttle Solid Rocket Booster (SRB) is a complex assembly of segments of which the field and factory joints contain an unpredictable amount of freeplay. Freeplay is inherent due to tolerances in being able to assemble the segments and the gaps that occur at each joint. The purpose of this work is to quantify the amount of freeplay for the field joint as well as identify the effects of introducing multiple joints that contain freeplay into a system. To provide a baseline for the above study an additional model was made to quantify the behavior of a field joint that does not have any freeplay in the system. Bodeker, Dan A., III and Foster, Windred A., Jr. Marshall Space Flight Center...
Book Synopsis Axisymmetric Shell Analysis of the Space Shuttle Solid Rocket Booster Field Joint by : Michael P. Nemeth
Download or read book Axisymmetric Shell Analysis of the Space Shuttle Solid Rocket Booster Field Joint written by Michael P. Nemeth and published by . This book was released on 1991 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Structural Optimization of an Alternate Design for the Space Shuttle Solid Rocket Booster Field Joint by :
Download or read book Structural Optimization of an Alternate Design for the Space Shuttle Solid Rocket Booster Field Joint written by and published by . This book was released on 1987 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722284503 Total Pages :58 pages Book Rating :4.2/5 (845 download)
Book Synopsis Axisymmetric Shell Analysis of the Space Shuttle Solid Rocket Booster Field Joint by : National Aeronautics and Space Administration (NASA)
Download or read book Axisymmetric Shell Analysis of the Space Shuttle Solid Rocket Booster Field Joint written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-08 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Space Shuttle Challenger (STS 51-L) accident led to an intense investigation of the structural behavior of the solid rocket booster (SRB) tang and clevis field joints. Results are presented of axisymmetric shell analyses that parametrically assess the structural behavior of SRB field joints subjected to quasi-steady-state internal pressure loading for both the original joint flown on mission STS 51-L and the redesigned joint flown for the first time after the STS 51-L accident on the Space Shuttle Discovery. Discussion of axisymmetric shell modeling issues and details is presented and a generic method for simulating contact between adjacent shells of revolution is described. Results are presented that identify the performance trends of the joints for a wide range of joint parameters. An important finding is that the redesigned joint exhibits significantly smaller O-ring gap changes and much less sensitivity to joint clearances than the original joint. For a wide range of joint parameters, the result presented indicate that the redesigned joint provides a much better pressure seal than the original joint. Nemeth, Michael P. and Anderson, Melvin S. Langley Research Center...
Book Synopsis Preliminary 2-D Shell Analysis of the Space Shuttle Solid Rocket Boosters by :
Download or read book Preliminary 2-D Shell Analysis of the Space Shuttle Solid Rocket Boosters written by and published by . This book was released on 1987 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Structural Analysis of a Bolted Joint Concept for the Space Shuttle's Solid Rocket Motor Casing by : Michael C. Lindell
Download or read book Structural Analysis of a Bolted Joint Concept for the Space Shuttle's Solid Rocket Motor Casing written by Michael C. Lindell and published by . This book was released on 1987 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Nonlinear Shell Analyses of the Space Shuttle Solid Rocket Boosters by :
Download or read book Nonlinear Shell Analyses of the Space Shuttle Solid Rocket Boosters written by and published by . This book was released on 1989 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Structural Analysis of the Space Shuttle Solid Rocket Booster/external Tank Attach Ring by :
Download or read book Structural Analysis of the Space Shuttle Solid Rocket Booster/external Tank Attach Ring written by and published by . This book was released on 1988 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722806309 Total Pages :32 pages Book Rating :4.8/5 (63 download)
Book Synopsis Structural Analysis of the Space Shuttle Solid Rocket Booster/External Tank Attach Ring by : National Aeronautics and Space Administration (NASA)
Download or read book Structural Analysis of the Space Shuttle Solid Rocket Booster/External Tank Attach Ring written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-11 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An External Tank (ET) attach ring is used in the Space Shuttle System to transfer lateral loads between the ET and the Solid Rocket Booster (SRB). Following the Challenger (51-L) accident, the flight performance of the ET attach ring was reviewed, and negative margins of safety and failed bolts in the attach ring were subsequently identified. The analyses described in this report were performed in order to understand the existing ET attach ring structural response to motor case internal pressurization as well as to aid in an ET attach ring redesign effort undertaken by NASA LaRC. The finite element model as well as the results from linear and nonlinear static structural analyses are described. Dorsey, John T. Langley Research Center RTOP 506-43-41-02...
Book Synopsis Lightweight Structural Design of a Bolted Case Joint for the Space Shuttle Solid Rocket Motor by : John T. Dorsey
Download or read book Lightweight Structural Design of a Bolted Case Joint for the Space Shuttle Solid Rocket Motor written by John T. Dorsey and published by . This book was released on 1988 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Structural Design of an In-line Bolted Joint for the Space Shuttle Solid Rocket Motor Case Segments by :
Download or read book Structural Design of an In-line Bolted Joint for the Space Shuttle Solid Rocket Motor Case Segments written by and published by . This book was released on 1987 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis System Analysis Approach to Deriving Design Criteria (loads) for Space Shuttle and Its Payloads. Volume 1: General Statement of Approach by : Robert Samuel Ryan
Download or read book System Analysis Approach to Deriving Design Criteria (loads) for Space Shuttle and Its Payloads. Volume 1: General Statement of Approach written by Robert Samuel Ryan and published by . This book was released on 1981 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Lightweight Structural Design of a Bolted Case Joint for the Space Shuttle Solid Rocket Motor by : John T. Dorsey
Download or read book Lightweight Structural Design of a Bolted Case Joint for the Space Shuttle Solid Rocket Motor written by John T. Dorsey and published by . This book was released on 1988 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report of the Presidential Commission on the Space Shuttle Challenger Accident by : DIANE Publishing Company
Download or read book Report of the Presidential Commission on the Space Shuttle Challenger Accident written by DIANE Publishing Company and published by DIANE Publishing. This book was released on 1995-07 with total page 267 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Vibration Characteristics of 1/8-scale Dynamic Models of the Space-shuttle Solid-rocket Boosters by :
Download or read book Vibration Characteristics of 1/8-scale Dynamic Models of the Space-shuttle Solid-rocket Boosters written by and published by . This book was released on 1976 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781792687648 Total Pages :34 pages Book Rating :4.6/5 (876 download)
Book Synopsis Effect of Temperature and Gap Opening Rate on the Resiliency of Candidate Solid Rocket Booster O-Ring Materials by : National Aeronautics and Space Adm Nasa
Download or read book Effect of Temperature and Gap Opening Rate on the Resiliency of Candidate Solid Rocket Booster O-Ring Materials written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2019 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the redesign of the Space Shuttle solid rocket motor following the Challenger accident, the field and nozzle-to-case joints were designed to minimize gap opening caused by internal motor pressurization during ignition. The O-ring seals and glands for these joints were designed both to accommodate structural deflections and to promote pressure assisted sealing. The resiliency behavior of several candidate O-ring materials was evaluated for the effects of temperature and gap opening rates. The performance of three of the elastomeric materials was tested under the specific redesign gap opening requirement. Dynamic flexure conditions unique to launch produce low frequency vibrations in the gap opening. The effect of these vibrations on the ability of the O-ring to maintain contact with the sealing surface was addressed. The resiliency of the O-ring materials was found to be extremely sensitive to variations in temperature and gap opening rate. The top three elastomeric materials tracked the simulated solid rocket booster (SRB) field joint deflection at 75 and 120 F. The external tank/SRB attach strut load vibrations had a negligible effect on the ability of the O-ring to track the simulated SRB field joint deflection. Lach, Cynthia L. Langley Research Center NASA-TP-3226, L-17023, NAS 1.60:3226 RTOP 505-63-50-03...
