Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Mehran Mobrem"'
Autor:
Manan Arya, Richard Hodges, Jonathan F. Sauder, Stephen Horst, Mehran Mobrem, Antonio Pedivellano, Alexander Wen, Alan Truong, Sergio Pellegrino
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
AIAA Scitech 2019 Forum.
Autor:
Mehran Mobrem, Lee D. Peterson
Publikováno v:
2018 AIAA Spacecraft Structures Conference.
Publikováno v:
4th AIAA Spacecraft Structures Conference.
Benchmarks are introduced for evaluating the performance of numerical simulations of space deployable structures. These benchmarks embody the key challenges of interest to future large space deployable structures, including large angle motion, contac
Autor:
Lee D. Peterson, Mehran Mobrem
Publikováno v:
4th AIAA Spacecraft Structures Conference.
Autor:
Mehran Mobrem, Douglas S. Adams
Publikováno v:
Journal of Spacecraft and Rockets. 46:394-402
DOI: 10.2514/1.36890 Extensive analytical and experimental activities were carried out that culminated in successful deployments in May and June of 2005 of three lenticular, jointed booms that formed a first of its kind of ground penetrating radar an
Autor:
Mehran Mobrem, Douglas S. Adams
Publikováno v:
Journal of Spacecraft and Rockets. 46:403-410
During the summer of 2005, ESAdeployed a series of three lenticular jointed antenna booms that formed afirst-ofits-kind ground-penetrating radar antenna onboard the Mars Express spacecraft. The booms were each released from their cradles with a high
Publikováno v:
2012 IEEE Aerospace Conference.
The Soil Moisture Active Passive1 (SMAP) instrument includes a conically scanning 6-m diameter deployable Astromesh reflector and feedhorn that rotates relative to a de-spun spacecraft at 14.6 RPM. This is the first application of a spinning Astromes
Autor:
Mehran Mobrem, Douglas S. Adams
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
This paper summarizes important milestones in a yearlong comprehensive effort which culminated in successful deployments of the MARSIS antenna booms in May and June of 2005. Experimentally measured straight section and hinge properties are incorporat
Autor:
Douglas S. Adams, Mehran Mobrem
Publikováno v:
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th.
This paper summarizes the resolution of an in flight anomaly that occurred during the deployment of the first of three MARSIS antenna booms. Characteristics of this deployment are described, along with a correlation to finite element models and measu