Zobrazeno 1 - 10
of 23
pro vyhledávání: '"M. Trubert"'
Publikováno v:
32nd Structures, Structural Dynamics, and Materials Conference.
A passive damping device intended to replace individual struts in precision truss structures for space applications is described. The theory of operation of the D-Strut device is detailed, and simple five- and three-parameter models are derived. Resu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d8a683b0de272e5e5da7aab03d18362
https://doi.org/10.2514/6.1991-996
https://doi.org/10.2514/6.1991-996
Publikováno v:
Journal of Sound and Vibration. 80:461-472
The second order nonlinear equations of motion are formulated for spinning line elements having little or no intrinsic structural stiffness. The derivation is based on the extended Hamilton's principle and includes the effect of initial geometric imp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::37b6c75c1f04489c49cb1b51a664e04b
https://doi.org/10.1016/0022-460x(82)90493-x
https://doi.org/10.1016/0022-460x(82)90493-x
Autor:
M. Trubert, Moktar Salama
Publikováno v:
AIAA Journal. 18:988-994
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9452dcaba419a3fb27a4bef7f350a55e
https://doi.org/10.2514/3.50843
https://doi.org/10.2514/3.50843
Publikováno v:
AIAA Journal. 22:824-830
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47d30100025f6d95cbfed458105421e8
https://doi.org/10.2514/3.8687
https://doi.org/10.2514/3.8687
Publikováno v:
27th Structures, Structural Dynamics and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e35e6dbc48c8004f30a607278a9f925b
https://doi.org/10.2514/6.1986-1002
https://doi.org/10.2514/6.1986-1002
Autor:
M. Trubert, R. Bamford
Publikováno v:
16th Structural Dynamics, and Materials Conference.
A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is developed. The method utilizes the interface shock spectra and the relative impedance of the spacecraft and launch vehicle. The method is developed for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed9696b2942059ba3f2343eb9396640d
https://doi.org/10.2514/6.1975-811
https://doi.org/10.2514/6.1975-811
Autor:
M. Trubert, M. Salama
Publikováno v:
20th Structures, Structural Dynamics, and Materials Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f04302ab3675f23b3a49bd8def347e8
https://doi.org/10.2514/6.1979-736
https://doi.org/10.2514/6.1979-736
Autor:
M. Salama, M. Trubert
Publikováno v:
20th Structures, Structural Dynamics, and Materials Conference.
Unlike the traditional shock spectra approach, the generalization presented in this paper permits elastic interaction between the spacecraft and launch vehicle in order to obtain accurate bounds on the spacecraft response and structural loads. In add
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de5784aee09e474ff7827e4b3f84ee3d
https://doi.org/10.2514/6.1979-745
https://doi.org/10.2514/6.1979-745
Autor:
J. Stevens, R. Goldstein, J. Kievit, E. Marsh, G. Varsi, M. Trubert, L. Stimpson, R. Landel, W. Rowe, W. Layman, W. Ruff, R. Ploszaj, W. Carroll, L. Friedman, J. Wright, R. Jacobson
Publikováno v:
16th Aerospace Sciences Meeting.
The practicability of using solar sails as a means of spacecraft propulsion is discussed with reference to a Haley's comet rendezvous mission in 1981. Two types of sails are examined: square and heliogyro. Because of ease of deployment (release into
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::02b5869048473493e14ebcf9350a62e9
https://doi.org/10.2514/6.1978-82
https://doi.org/10.2514/6.1978-82
Autor:
L. Peretti, M. Trubert
Publikováno v:
26th Structures, Structural Dynamics, and Materials Conference.
A combination of the time and frequency domains which employs the latter only where the former is inefficient or uncertain is used in Space Shuttle payloads' component mode analyses. Attention is given to the time histories at the launch vehicle/spac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54ee2ad6b5d2bfbdabf4dccf71fc0eb0
https://doi.org/10.2514/6.1985-733
https://doi.org/10.2514/6.1985-733