Jul 2026· 55th International Conference on Environmental Systems· 0 citations
Abstract
The gravity on Mars is 3/8th of Earth gravity. The latest exploration Extravehicular Mobility Unit (xEMU) designed for lunar exploration is just under 400 lbm. While it would be reasonable for a crewmember to operate the xEMU on Earth’s Moon with 1/6 gravity, related studies have demonstrated that this same suit would not be feasible to operate on the surface on Mars. Studies involving Martian offloading are limited and the few available have demonstrated difficulty in suit operation with current advanced suit prototypes. Furthermore, deconditioning due to a long-term journey to Mars is expected to affect the overall suit mass that a crewmember can operate. This initial study aims to provide an initial mass requirement to bound the Mars spacesuit design within a reasonable range. It is expected that detailed Mars-simulation testing will subsequently refine the estimate to support Martian mission timelines. Considerations such as crew deconditioning due to the long exposure to microgravity, pressure garment system (PGS) weight offloading, restricted mobility increasing metabolic rate, and human fitness and size are combined into an initial assessment. Based on preliminary considerations, 230 lbm is recommended as a starting maximum Mars suit mass, which will be split between the PGS and Portable Life Support System (PLSS) subsystems.
Close-proximity exploration of airless celestial bodies is challenging due to low gravity, lack of atmosphere, and uncertain surface properties. The “E-Glider”, conceived by Dr. Quadrelli, is a promising concept to overcome these obstacles and enable detailed exploration in these environments. Their working mechanism r...
Jesús Manuel Muñoz Tejeda, Bruno Marco Quadrelli· Journal of Electric Propulsi...· 0 citations
This work is part of the BIS Orbital Settlement technical project, which is studying near-term possibilities for an expansion of industrial civilisation, on Earth and in space. This will be facilitated by the construction of large orbital habitats in jig- factories. This paper describes the launch and orbital transfer...
R. Soilleux· JBIS - Journal of the Britis...· 0 citations
The Gravitational Reference Advanced Technology Test In Space (GRATTIS) mission will demonstrate the functionality and sensitivity performance of the Simplified Gravitational Reference Sensor (S-GRS), an ultra-precise inertial sensor for future Earth geodesy missions. These sensors are used to measure or compensate for...
John W. Conklin· GRACE/GRACE-FO Science Team...· 0 citations
The Emirates Mission to the Asteroid Belt (EMA), scheduled for launch in 2028, will conduct an eight-year, multi-target tour of seven main-belt asteroids, requiring over 10 km/s total delta-v and operations out to 3 AU. To meet these demands, the Laboratory for Atmospheric and Space Physics (LASP), in partnership with...
S. Green, B. Reese, R. Riley et al.· Journal of Electric Propulsi...· 0 citations
The Earth 2.0 (ET) mission is a next-generation Chinese space mission aimed at detecting thousands of Earth-sized planets, including habitable Earth-like planets around solar-type stars (Earth 2.0s), cold low-mass planets, and free-floating planets. ET will carry six 28 cm transit telescopes, each with a 550 deg² field...
Kun Chen, Wen Chen, Ying-Quan Yang et al.· Astronomical Telescopes + In...· 0 citations
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