Cyclic Cryogenic Thermal-Mechanical Testing of an X-33/RLV Liquid Oxygen Tank Concept PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Cyclic Cryogenic Thermal-Mechanical Testing of an X-33/RLV Liquid Oxygen Tank Concept PDF full book. Access full book title Cyclic Cryogenic Thermal-Mechanical Testing of an X-33/RLV Liquid Oxygen Tank Concept by H. Kevin Rivers. Download full books in PDF and EPUB format.
Author: H. Kevin Rivers
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 20
Get Book Here
Book Description
Author: H. Kevin Rivers
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 20
Get Book Here
Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721190027
Category :
Languages : en
Pages : 32
Get Book Here
Book Description
An important step in developing a cost-effective, reusable, launch vehicle is the development of durable, lightweight, insulated, cryogenic propellant tanks. Current cryogenic tanks are expendable so most of the existing technology is not directly applicable to future launch vehicles. As part of the X-33/Reusable Launch Vehicle (RLV) Program, an experimental apparatus developed at the NASA Langley Research Center for evaluating the effects of combined, cyclic, thermal and mechanical loading on cryogenic tank concepts was used to evaluate cryogenic propellant tank concepts for Lockheed-Martin Michoud Space Systems. An aluminum-lithium (Al 2195) liquid oxygen tank concept, insulated with SS-1171 and PDL-1034 cryogenic insulation, is tested under simulated mission conditions, and the results of those tests are reported. The tests consists of twenty-five simulated Launch/Abort missions and twenty-five simulated flight missions with temperatures ranging from -320 F to 350 F and a maximum mechanical load of 71,300 lb. in tension. Rivers, H. Kevin Langley Research Center NASA/TM-1999-209560, L-17818, NAS 1.15:209560
Author: H. Kevin Rivers
Publisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 13
Get Book Here
Book Description
Author: H.Kevin Rivers
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 182
Get Book Here
Book Description
Author: Committee on Reusable Launch Vehicle Technology and Test Program
Publisher: National Academies Press
ISBN: 0309588960
Category : Science
Languages : en
Pages : 99
Get Book Here
Book Description
The key to opening the use of space to private enterprise and to broader public uses lies in reducing the cost of the transportation to space. More routine, affordable access to space will entail aircraft-like quick turnaround and reliable operations. Currently, the space Shuttle is the only reusable launch vehicle, and even parts of it are expendable while other parts require frequent and extensive refurbishment. NASA's highest priority new activity, the Reusable Launch Vehicle program, is directed toward developing technologies to enable a new generation of space launchers, perhaps but not necessarily with single stage to orbit capability. This book assesses whether the technology development, test and analysis programs in propulsion and materials-related technologies are properly constituted to provide the information required to support a December 1996 decision to build the X-33, a technology demonstrator vehicle; and suggest, as appropriate, necessary changes in these programs to ensure that they will support vehicle feasibility goals.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 658
Get Book Here
Book Description
Author: Seth Stovack Kessler
Publisher:
ISBN:
Category :
Languages : en
Pages : 25
Get Book Here
Book Description
With many new space programs on the horizon, driving the cost of space payload down has become a major topic in the aerospace industry. One approach taken by the structural engineer to reduce this cost is to replace metallic sections of a vehicle with more advanced materials such as composites. This project addresses various issues involved with replacing the fuel tank of a space vehicle with advanced composites. These tanks operate at cryogenic temperatures producing large strains through the layers of the composite, and additionally they must be able to endure several cycles of thermal loading at both extremes without leaking fuel. The particular composite studied in this project was IM7-977-2, a graphite fiber with toughened epoxy, which is being used for the Lockheed Martin Skunk Work's X-33. This project explores the degradation of the composite's mechanical properties due to cryocycling, and attempts to establish the mechanism behind the degradation through a non-destructive crack density analysis.
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309266564
Category : Science
Languages : en
Pages : 115
Get Book Here
Book Description
On June 15, 2011, the Air Force Space Command established a new vision, mission, and set of goals to ensure continued U.S. dominance in space and cyberspace mission areas. Subsequently, and in coordination with the Air Force Research Laboratory, the Space and Missile Systems Center, and the 14th and 24th Air Forces, the Air Force Space Command identified four long-term science and technology (S&T) challenges critical to meeting these goals. One of these challenges is to provide full-spectrum launch capability at dramatically lower cost, and a reusable booster system (RBS) has been proposed as an approach to meet this challenge. The Air Force Space Command asked the Aeronautics and Space Engineering Board of the National Research Council to conduct an independent review and assessment of the RBS concept prior to considering a continuation of RBS-related activities within the Air Force Research Laboratory portfolio and before initiating a more extensive RBS development program. The committee for the Reusable Booster System: Review and Assessment was formed in response to that request and charged with reviewing and assessing the criteria and assumptions used in the current RBS plans, the cost model methodologies used to fame [frame?] the RBS business case, and the technical maturity and development plans of key elements critical to RBS implementation. The committee consisted of experts not connected with current RBS activities who have significant expertise in launch vehicle design and operation, research and technology development and implementation, space system operations, and cost analysis. The committee solicited and received input on the Air Force launch requirements, the baseline RBS concept, cost models and assessment, and technology readiness. The committee also received input from industry associated with RBS concept, industry independent of the RBS concept, and propulsion system providers which is summarized in Reusable Booster System: Review and Assessment.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1048
Get Book Here
Book Description
