Zobrazeno 1 - 10
of 45
pro vyhledávání: '"Jamshid A. Samareh"'
Publikováno v:
ASCEND 2021.
Publikováno v:
Journal of Spacecraft and Rockets. 56:1742-1756
Cost is one of the biggest obstacles to sending humans to Mars. However, spacecraft costs are typically not estimated until after the preliminary vehicle and mission concepts have been designed. By...
Autor:
Paul D. Friz, Jamshid A. Samareh
Publikováno v:
ASCEND 2020.
Cost is one of the biggest obstacles to sending humans to Mars. However, spacecraft costs are typically estimated after the preliminary vehicle and mission concepts have been designed. By automating the cost estimation process, the effect of any chan
Autor:
Jamshid A. Samareh
Publikováno v:
AIAA Scitech 2020 Forum.
Publikováno v:
Journal of Spacecraft and Rockets. 55:1379-1392
The Tension Adjustable Network for Deploying Entry Membrane (TANDEM) is a tensegrity rover designed to also be the frame of a deployable heat shield. TANDEM integrates the heatshield technology dev...
Publikováno v:
Journal of Spacecraft and Rockets. 55:561-574
An in-depth investigation of the structural design of the Venera landers was explored. A reverse engineering of the Venera-class lander was performed. The lander was broken down into its fundamenta...
Publikováno v:
2018 AIAA SPACE and Astronautics Forum and Exposition.
Cost is one of the biggest obstacles to sending humans to Mars. However, spacecraft costs are typically not estimated until after the preliminary vehicle and mission concepts have been designed. By automating the cost estimation process, the effect o
Autor:
Eddie Krutyanskiy, Jacob Walder, Aaron Knust, Ian Stewart, Tommy Cleckner, Greta Ostergaard, Christopher Nickles, Aldo Morales, Jamshid A. Samareh, Maximilian Moller, Robert Zakotnik
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Publikováno v:
Journal of Spacecraft and Rockets. 52:1320-1330
A parametric structural investigation of a new atmospheric entry vehicle concept for future planetary probes and sample return vehicles was conducted. During launch and reentry, the vehicle may experience large structural loads. To enable rapid asses
Publikováno v:
Journal of Spacecraft and Rockets. 52:1217-1227
Development of an Earth entry vehicle and the methodology created to evaluate the vehicle’s impact landing response when returning to Earth is reported. NASA’s future Mars Sample Return Mission requires a robust vehicle to return Martian samples