[图书][B] Human missions to Mars
D Rapp - 2007 - Springer
Human missions to Mars represent the pinnacle of solar system exploration for the next half-
century. In addition to providing an exploration of Mars, such missions would represent an …
century. In addition to providing an exploration of Mars, such missions would represent an …
Entry, Descent, and Landing technological barriers and crewed MARS vehicle performance analysis
P Subrahmanyam, D Rasky - Progress in Aerospace Sciences, 2017 - Elsevier
Mars has been explored historically only by robotic crafts, but a crewed mission
encompasses several new engineering challenges–high ballistic coefficient entry …
encompasses several new engineering challenges–high ballistic coefficient entry …
Initial assessment of Mars Science Laboratory heatshield instrumentation and flight data
D Bose, M Olson, B Laub, T White, J Feldman… - 51st AIAA Aerospace …, 2013 - arc.aiaa.org
Abstract The Mars Science Laboratory (MSL) Entry Descent and Landing Instrumentation
(MEDLI) suite on MSL entry vehicle heatshield has successfully returned pressure …
(MEDLI) suite on MSL entry vehicle heatshield has successfully returned pressure …
Development of supersonic retropropulsion for future mars entry, descent, and landing systems
KT Edquist, AM Korzun, AA Dyakonov… - Journal of Spacecraft …, 2014 - arc.aiaa.org
STARTING with the two Viking landers in 1976 and continuing through the successful Mars
Science Laboratory [1](MSL) landing in 2012, NASA and its partners have used similar …
Science Laboratory [1](MSL) landing in 2012, NASA and its partners have used similar …
An overview of ball flash LiDAR and related technology development
R Rohrschneider, J Masciarelli, KL Miller… - … , Navigation, and Control …, 2013 - arc.aiaa.org
There are many space navigations tasks that can benefit from 3D point cloud data, including
rendezvous and docking, precision landing, spacecraft servicing, and space surveillance …
rendezvous and docking, precision landing, spacecraft servicing, and space surveillance …
Zirconium-doped hybrid composite systems for ultrahigh-temperature oxidation applications: a review
G Gudivada, B Kandasubramanian - Industrial & Engineering …, 2019 - ACS Publications
The re-entry phase of a space vehicle demands thermal shielding against the heat elicited
by an aerodynamic heating process. The quantity of heat spawned in such process is close …
by an aerodynamic heating process. The quantity of heat spawned in such process is close …
Mars science laboratory heat shield instrumentation and arc jet characterization
D Bose, JA Santos, E Rodriguez, TR White… - 44th AIAA …, 2013 - arc.aiaa.org
Abstract The Mars Science Laboratory (MSL) Entry Descent and Landing Instrumentation
(MEDLI) suite on MSL entry vehicle heatshield has returned pressure, temperature, and …
(MEDLI) suite on MSL entry vehicle heatshield has returned pressure, temperature, and …
[图书][B] Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent
AM Korzun - 2012 - search.proquest.com
The entry, descent, and landing (EDL) systems for the United States' six successful landings
on Mars and the 2011 Mars Science Laboratory (MSL) have all relied heavily on extensions …
on Mars and the 2011 Mars Science Laboratory (MSL) have all relied heavily on extensions …
Touchdown Dynamics and the Probability of Terrain Related Failure of Planetary Landing Systems-A Contribution to the Landing Safety Assessment Process
L Witte - 2015 - elib.dlr.de
Landing safety assessment is an integral element of the planning of a landing mission. This
thesis contributes to such assessment with the modelling and deduction of the functional …
thesis contributes to such assessment with the modelling and deduction of the functional …
Design of a novel hypersonic inflatable aerodynamic decelerator for mars entry, descent, and landing
N Skolnik, H Kamezawa, L Li, GA Rossman… - AIAA Atmospheric …, 2017 - arc.aiaa.org
Entry, descent, and landing (EDL) is especially challenging on Mars due the nature of the
planet. The atmosphere on Mars is too thin (approximately 1% of Earth's density) to provide …
planet. The atmosphere on Mars is too thin (approximately 1% of Earth's density) to provide …