3 edition of Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes found in the catalog.
Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes
Published
1984
by National Aeronautics and Space Administration, Scientific and Technical Information Branch in [Washington, D.C.?]
.
Written in English
Edition Notes
Statement | Huey D. Carden |
Series | NASA technical paper -- 2380 |
Contributions | United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch |
The Physical Object | |
---|---|
Format | Microform |
Pagination | 1 v. |
ID Numbers | |
Open Library | OL14933657M |
Analysis of programs of state aid to local governments in Maryland
Creative naval architecture
Marvelous Misadventures of Sebastian, Th
Jet lag and travel
Assessing the validity of event markers in multiple myeloma
Studies of the labour market and the labour process with special reference to the Oxford region
Caring for Children - Families
Openboot 3.X Command Reference Manual
You Can Go Home Again - And Other Thoughts About Changing Your Life
Metal physics
Neutralizing the nuclear and radiological threat
Full scale crash-test evaluation of two load-limiting subfloors for general aviation airframes. NASA Technical PaperLangley Research Cited by: 7. Get this from a library. Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes.
[Huey D Carden; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.]. Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes [microfor Evaluation of energy absorption of new concepts of aircraft composite subfloor intersections [microform] Unique failure behavior of metal/composite aircraft structural components under crash type loads [microf.
The Aging Aircraft Safety Act [microform]: hearing before the Subcommittee on Aviation of the Committee Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes [microfor.
In the s, the U.S. general aviation industry nearly collapsed. At its peak inthe U.S. general aviation industry delive aircraft. Inthe number of aircraft deliveries had fallen to an all-time low of The average age of general aviation aircraft flying at that time was about 30 years.5/5(2).
A large number of full scale tests of general aviation aircraft, helicopters, and one unique air-to-ground controlled impact of a transport aircraft were performed. Additionally, research was also conducted on seat dynamic performance, load-limiting seats, load limiting subfloor designs, and emergency-locator-transmitters (ELTs).
[] "Full-Scale Transport Controlled Impact Demonstration Program: Final Summary Report,’ NASA TM (Sept. ), p. "Full-Scale Crash-Test Evaluation of Two Load-Limiting Subfloors for General Aviation Airframes," NASA TP ().
A research team equipped the vintage airplanes with five ELTs, two crash test dummies, cameras and data-collecting sensors. ELTs are installed on general aviation and commercial planes to transmit a location signal in the event of a crash. Current ELT models send that signal to orbiting satellites, which repeat it to the nearest search and.
Full text of "NASA scientific and technical publications: A catalog of Special Publications, Reference Publications, Conference Publications, and. An illustration of an open book.
Books. An illustration of two cells of a film strip. Video. An illustration of an audio speaker. Audio. An illustration of a " floppy disk. Software. An illustration of two photographs. Images.
An illustration of a heart .