Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix G: Lrb for the Sts System Study Level 2 Requirements, Re

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix G: Lrb for the Sts System Study Level 2 Requirements, Re PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781731366856
Category : Science
Languages : en
Pages : 160

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Book Description
Requirements are presented for shuttle system definition; performance and design characteristics; shuttle vehicle end item performance and design characteristics; ground operations complex performance and design characteristics; operability and system design and construction standards; and quality control. BOOSTER ROCKET ENGINES; DEFINITION; DESIGN ANALYSIS; SPACE TRANSPORTATION SYSTEM; STANDARDS; SYSTEMS ANALYSIS; CONSTRUCTION; GROUND OPERATIONAL SUPPORT SYSTEM; QUALITY CONTROL; SPACECRAFT PERFORMANCE...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix G: Lrb for the Sts System Study Level 2 Requirements, Re

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix G: Lrb for the Sts System Study Level 2 Requirements, Re PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781731366856
Category : Science
Languages : en
Pages : 160

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Book Description
Requirements are presented for shuttle system definition; performance and design characteristics; shuttle vehicle end item performance and design characteristics; ground operations complex performance and design characteristics; operability and system design and construction standards; and quality control. BOOSTER ROCKET ENGINES; DEFINITION; DESIGN ANALYSIS; SPACE TRANSPORTATION SYSTEM; STANDARDS; SYSTEMS ANALYSIS; CONSTRUCTION; GROUND OPERATIONAL SUPPORT SYSTEM; QUALITY CONTROL; SPACECRAFT PERFORMANCE...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix G

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix G PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723194757
Category :
Languages : en
Pages : 158

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Book Description
Requirements are presented for shuttle system definition; performance and design characteristics; shuttle vehicle end item performance and design characteristics; ground operations complex performance and design characteristics; operability and system design and construction standards; and quality control. Unspecified Center BOOSTER ROCKET ENGINES; DEFINITION; DESIGN ANALYSIS; SPACE TRANSPORTATION SYSTEM; STANDARDS; SYSTEMS ANALYSIS; CONSTRUCTION; GROUND OPERATIONAL SUPPORT SYSTEM; QUALITY CONTROL; SPACECRAFT PERFORMANCE...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix a

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix a PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781729367711
Category :
Languages : en
Pages : 56

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Book Description
Pressure effects on the pump-fed Liquid Rocket Booster (LRB) of the Space Transportation System are examined. Results from the buckling tests; bending moments tests; barrel, propellant tanks, frame XB1513, nose cone, and intertank tests; and finite element examination of forward and aft skirts are presented. Unspecified Center...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix B: Liquid Rocket Booster Acoustic and Thermal Environmen

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Appendix B: Liquid Rocket Booster Acoustic and Thermal Environmen PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781729308394
Category : Science
Languages : en
Pages : 52

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Book Description
The ascent thermal environment and propulsion acoustic sources for the Martin-Marietta Corporation designed Liquid Rocket Boosters (LRB) to be used with the Space Shuttle Orbiter and External Tank are described. Two designs were proposed: one using a pump-fed propulsion system and the other using a pressure-fed propulsion system. Both designs use LOX/RP-1 propellants, but differences in performance of the two propulsion systems produce significant differences in the proposed stage geometries, exhaust plumes, and resulting environments. The general characteristics of the two designs which are significant for environmental predictions are described. The methods of analysis and predictions for environments in acoustics, aerodynamic heating, and base heating (from exhaust plume effects) are also described. The acoustic section will compare the proposed exhaust plumes with the current SRB from the standpoint of acoustics and ignition overpressure. The sections on thermal environments will provide details of the LRB heating rates and indications of possible changes in the Orbiter and ET environments as a result of the change from SRBs to LRBs. Unspecified Center NAS8-37136...

Liquid Rocket Booster (Lrb) for the Space Transportion System (Sts) Systems Study. Appendix D

Liquid Rocket Booster (Lrb) for the Space Transportion System (Sts) Systems Study. Appendix D PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722617202
Category :
Languages : en
Pages : 60

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Book Description
Trade studies plans for a number of elements in the Liquid Rocket Booster (LRB) component of the Space Transportation System (STS) are given in viewgraph form. Some of the elements covered include: avionics/flight control; avionics architecture; thrust vector control studies; engine control electronics; liquid rocket propellants; propellant pressurization systems; recoverable spacecraft; cryogenic tanks; and spacecraft construction materials. Unspecified Center...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Volume 1

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Volume 1 PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722616915
Category :
Languages : en
Pages : 56

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Book Description
The feasibility of replacing the Space Transportation System (STS) Solid Rocket Boosters (SRBs) with Liquid Rocket Boosters (LRBs) was studied. Feasibility required acceptable technical risk, program costs, and a program plan which supports STS requirements. Three major goals were identified to direct booster design and operation: increased STS safety and reliability; STS/LRB integration with minimum impact; and increased STS performance. Two booster engine designs were studied. The first engine design was a turbopump-fed engine with state-of-the-art design, and the second was a pressure-fed engine which might provide a lower cost alternative to the pump-fed concept. Both booster concepts were carried through to completion of conceptual design and all system impacts and program costs were identified. Applications for LRB use in the Advanced Launch System (ALS) program were studied using the pump-fed LRB baseline concept and variations on the baseline concept. Support for the Pressure-Fed Booster Test Bed (PFBTB) included test program planning and costs and technical support. Unspecified Center...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Volume 1

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study. Volume 1 PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781729367841
Category :
Languages : en
Pages : 56

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Book Description
The feasibility of replacing the Space Transportation System (STS) Solid Rocket Boosters (SRBs) with Liquid Rocket Boosters (LRBs) was studied. Feasibility required acceptable technical risk, program costs, and a program plan which supports STS requirements. Three major goals were identified to direct booster design and operation: increased STS safety and reliability; STS/LRB integration with minimum impact; and increased STS performance. Two booster engine designs were studied. The first engine design was a turbopump-fed engine with state-of-the-art design, and the second was a pressure-fed engine which might provide a lower cost alternative to the pump-fed concept. Both booster concepts were carried through to completion of conceptual design and all system impacts and program costs were identified. Applications for LRB use in the Advanced Launch System (ALS) program were studied using the pump-fed LRB baseline concept and variations on the baseline concept. Support for the Pressure-Fed Booster Test Bed (PFBTB) included test program planning and costs and technical support. Unspecified Center...

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study

Liquid Rocket Booster (Lrb) for the Space Transportation System (Sts) Systems Study PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724278586
Category :
Languages : en
Pages : 302

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Book Description
The Liquid Rocket Booster (LRB) Systems Definition Handbook presents the analyses and design data developed during the study. The Systems Definition Handbook (SDH) contains three major parts: the LRB vehicles definition; the Pressure-Fed Booster Test Bed (PFBTB) study results; and the ALS/LRB study results. Included in this volume are the results of all trade studies; final configurations with supporting rationale and analyses; technology assessments; long lead requirements for facilities, materials, components, and subsystems; operational requirements and scenarios; and safety, reliability, and environmental analyses. Unspecified Center NASA-CR-183786, NAS 1.26:183786 NAS8-37136...

Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study; Volume 1 - Executive Summary

Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study; Volume 1 - Executive Summary PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Book Description
In October 1987, NASA/MSFC awarded Martin Marietta Manned Space Systems a contract to study the feasibility of replacing the Space Transportation System (STS) solid rocket boosters (SRBs) with liquid rocket boosters (LRBs), Figure 1.0-1. The main objectives of a LRB substitution for the SRB were increased STS safety and reliability and increased payload performance to 70.5K lb to low earth orbit (LEO) with minimum impacts to the STS. The basic scope of work was directed to the definition of optimum liquid rocket booster concepts for replacing SRB's within the current STS operational constraints and envelopes. The initial contract was phased in two parts. Part 1 was designated for establishment of a baseline configuration and system trade studies. Part 2 further defined the baseline, incorporating the results of the trade studies and preliminary analyses which were performed on the various systems. Life cycle costs (LCC) were developed for the program and new technology requirements were identified. In July, 1988 a six month extension, Part 3, of the study was awarded so that concepts could be further optimized, alternate applications for LRB could be explored, and planning and technical support for a pressure-fed propulsion system test bed could be provided. Figure 1.0-2 illustrates the LRB definition study flow. Two booster engine designs were studied. The first engine design was a turbo pump-fed engine with state-of-the-art design, and the second was a pressure-fed engine which might provide a lower cost alternative to the pump-fed concept. Both booster concepts were carried through to completion of conceptual design and all system impacts and program costs were identified.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.