Zobrazeno 1 - 10
of 17
pro vyhledávání: '"John E. Higgins"'
Publikováno v:
Hydrobiologia. 690:189-197
The jellyfish Drymonema larsoni bloomed in the northern Gulf of Mexico in the Fall of 2000 and fed voraciously on the moon jellyfish Aurelia sp., especially where they were concentrated in frontal convergence. We evaluated the predation potential of
Autor:
Barry VanWest, John E. Higgins
Publikováno v:
Composite Structures. 67:189-195
A composite grid-stiffened structural concept was selected for the payload fairing of the Minotaur launch vehicle. Compared to sandwich structures, this concept has the advantages of lower manufacturing costs and lighter weight. Various failure modes
Publikováno v:
Jellyfish Blooms IV ISBN: 9789400753150
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::80aaeff87bc09c2df6ac1ea105225145
https://doi.org/10.1007/978-94-007-5316-7_15
https://doi.org/10.1007/978-94-007-5316-7_15
Autor:
Jerome Berg, John E. Higgins, Chris Springer, Steven A. Lane, Adam Biskner, Gregory E. Sanford
Publikováno v:
Journal of Manufacturing Science and Engineering. 133
This paper documents a recent R&D effort conducted by the Air Force Research Laboratory, Space Vehicles Directorate, to assess the feasibility of fabricating large composite launch vehicle fairings without the use of autoclaves. Two composite manufac
Autor:
Tomoya Ochinero, Thomas A. Deiters, Eric Blades, Brandon Arritt, John E. Higgins, James C. Newman
Publikováno v:
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A very large asymmetric composite payload fairing (PLF) was developed for launching payloads of unconventional geometry and size on the Atlas V Heavy Lift vehicle. Currently, no launch system exists that can accommodate these payloads without requiri
Publikováno v:
49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 16th AIAA/ASME/AHS Adaptive Structures Conference 10t.
This paper describes the development and testing of a new fairing for the Minotaur IV launch vehicle that increases the nominal diameter by 20 percent to 110 inches. The Air Force Research Laboratory's Space Vehicles Directorate managed the developme
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
[Abstract] The Access to Space initiative is providing the incentive for launching increasingly large payloads. Composites are an excellent choice for the launch vehicle structure to carry these large payloads, as a result of low mass density and hig
Publikováno v:
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Autor:
Cole K. Corbin, John E. Higgins
Publikováno v:
Earth & Space 2006.
Autor:
John E. Higgins, Adam Biskner
Publikováno v:
46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference.
A composite grid-stiffened structure concept was selected for the payload fairing of the Minotaur launch vehicle. Compared to previous designs, this concept is lighter weight and requires reduced manufacturing costs. Various failure mechanisms were e