A review of multifunctional structure technology for aerospace applications

KK Sairajan, GS Aglietti, KM Mani - Acta astronautica, 2016 - Elsevier
The emerging field of multifunctional structure (MFS) technologies enables the design of
systems with reduced mass and volume, thereby improving their overall efficiency. It …

Flash converted graphene for ultra‐high power supercapacitors

LJ Wang, MF El‐Kady, S Dubin… - Advanced Energy …, 2015 - Wiley Online Library
Supercapacitors are known for their rapid energy charge–discharge properties, often ten to
a hundred times faster than batteries. However, there is still a demand for supercapacitors …

Thermal behavior of heat-pipe-assisted alkali-metal thermoelectric converters

JS Lee, WH Lee, RG Chi, WS Chung, KB Lee… - Heat and Mass …, 2017 - Springer
The alkali-metal thermal-to-electric converter (AMTEC) changes thermal energy directly into
electrical energy using alkali metals, such as sodium and potassium, as the working fluid …

Analysis of Proposed Active Radiation Shielding Design Concept for Spacecraft

C Mechmann - 2022 - repository.fit.edu
A need exists to protect the crew of interplanetary spacecraft from lethal doses of Galactic
Cosmic Radiation (GCR) and Solar Energetic Particles (SEPs). As plans progress to send …

[图书][B] Nanosatellite electrical power system development

N Navarathinam - 2010 - collectionscanada.gc.ca
Nanosatellites have the potential to carry out the complex work of today's larger satellites at
a fraction of the cost. Their small designs drastically reduce launch costs and allow many …

Low-Thrust Control of a Lunar Mapping Orbit

N Harl, HJ Pernicka - Journal of guidance, control, and dynamics, 2009 - arc.aiaa.org
A method is presented for establishing and maintaining a lunar mapping orbit using
continuous-low-thrust propulsion. Optimal control theory is used to maintain a lunar orbit that …

Review of micro-autonomous vehicle sizing and power modeling

R Mukherjee, M Heiges… - … Sensors, Systems, and …, 2010 - spiedigitallibrary.org
This paper presents a discussion on sizing, weight and power of micro autonomous air and
ground vehicles. While the air vehicles include both rotor and flapper based design, here the …

Limits to rover miniaturisation and their implications for solar system exploration

S Edwards - arXiv preprint arXiv:1706.05356, 2017 - arxiv.org
Semiautonomous rover scaling is examined for exploration throughout the solar system.
Communications to a relay orbiter is a major constraint, due to power requirements and …

Analysis of an Energy Storage System Based on Regenerative Fuel Cells for Spacecraft

D Rosenberg, D Pinto, I Schnitzer - 57th International Astronautical …, 2006 - arc.aiaa.org
In the last year Israel Aircraft Industries (IAI) has engaged in the study of Proton Exchange
Membrane (PEM) based Regenerative Fuel Cells (RFC) technology for electrical energy …

Space Power Trends

G Spanjers, T Roberts - Encyclopedia of Aerospace …, 2010 - Wiley Online Library
Size and performance characteristic limits are discussed for government and commercial
spacecraft classes. Potential future sources of space power are described. These …