Provenance
Source & edition record
This page records where the text came from, what changed in presentation, and what remains unverified.
Bibliographic source
- Work
- Hot/Wet Open Hole Compression Strength of Carbon/Epoxy Laminates for Launch Vehicle Applications
- Author
- Alan T. Nettles
- First publication
- NASA Technical Reports Server
- Source edition
- Technical Memorandum (TM), NASA, 2009
- Accessed
- 2026-08-24
- Verification
- source-compared
- Source snapshot SHA-256
a07a420f5df0cbf1bfb57c3a08a228b8033b978429a0a98814e5fc28210ff4f7
Transformations
Rights status
public-domain. NASA NTRS marks this record as a work of the U.S. Government with public use permitted and no third-party material indicated. View the rights record ↗