NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Task 4 supporting technology. Part 2: Detailed test plan for thermal seals. Thermal seals evaluation, improvement and test. CAN8-1, Reusable Launch Vehicle (RLV), advanced technology demonstrator: X-33. Leading edge and seals thermal protection system technology demonstrationThe objective is to develop the advanced thermal seals to a technology readiness level (TRL) of 6 to support the rapid turnaround time and low maintenance requirements of the X-33 and the future reusable launch vehicle (RLV). This program is divided into three subtasks: (1) orbiter thermal seals operation history review; (2) material, process, and design improvement; and (3) fabrication and evaluation of the advanced thermal seals.
Document ID
19950021838
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hogenson, P. A. (Rockwell International Corp. Downey, CA, United States)
Lu, Tina (Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 30, 1995
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-198628
NAS 1.26:198628
SSD95D0240-PT-2
Report Number: NASA-CR-198628
Report Number: NAS 1.26:198628
Report Number: SSD95D0240-PT-2
Accession Number
95N28259
Funding Number(s)
CONTRACT_GRANT: NCC8-79
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available