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High-speed civil transport issues and technology programA strawman program plan is presented, consisting of technology developments and demonstrations required to support the construction of a high-speed civil transport. The plan includes a compilation of technology issues related to the development of a transport. The issues represent technical areas in which research and development are required to allow airframe manufacturers to pursue an HSCT development. The vast majority of technical issues presented require flight demonstrated and validated solutions before a transport development will be undertaken by the industry. The author believes that NASA is the agency best suited to address flight demonstration issues in a concentrated effort. The new Integrated Test Facility at NASA Dryden Flight Research Facility is considered ideally suited to the task of supporting ground validations of proof-of-concept and prototype system demonstrations before night demonstrations. An elaborate ground hardware-in-the-loop (iron bird) simulation supported in this facility provides a viable alternative to developing an expensive fill-scale prototype transport technology demonstrator. Drygen's SR-71 assets, modified appropriately, are a suitable test-bed for supporting flight demonstrations and validations of certain transport technology solutions. A subscale, manned or unmanned flight demonstrator is suitable for flight validation of transport technology solutions, if appropriate structural similarity relationships can be established. The author contends that developing a full-scale prototype transport technology demonstrator is the best alternative to ensuring that a positive decision to develop a transport is reached by the United States aerospace industry.
Document ID
19920021964
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hewett, Marle D.
(G and C Systems, Inc. San Juan Capistrano, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:186020
H-1795
NASA-CR-186020
Report Number: NAS 1.26:186020
Report Number: H-1795
Report Number: NASA-CR-186020
Accession Number
92N31208
Funding Number(s)
CONTRACT_GRANT: NAS2-12722
PROJECT: RTOP 505-64-20
CONTRACT_GRANT: ATD-91-GNC-7102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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