Solar sailing CubeSat attitude control method with satellite as moving mass

H Huang, J Zhou - Acta Astronautica, 2019 - Elsevier
Low-cost solar sailing CubeSats for deep-space exploration are relatively inexpensive, have
a short development time, and can be launched more often. However, attitude control of a …

[HTML][HTML] Solar-sail mission design for multiple near-Earth asteroid rendezvous

A Peloni - 2018 - theses.gla.ac.uk
Solar sailing is the use of a thin and lightweight membrane to reflect sunlight and obtain a
thrust force on the spacecraft. That is, a sailcraft has a potentially-infinite specific impulse …

Integrating model-based systems engineering and value-based design with an NEA scout small satellite example

G Bhatia, B Mesmer - AIAA SPACE and Astronautics Forum and …, 2017 - arc.aiaa.org
ARGE-SCALE complex engineered systems (LSCES) are characterized by the extensive
number of individuals participating in designing the system, the complex interactions …

[图书][B] Innovations in pulsed plasma thrusters to enable CubeSat science missions

P Northway - 2020 - search.proquest.com
CubeSats and other small satellites in the 3-25 kg range are increasingly able to conduct
meaningful science through advances in technology and miniaturization. However, much of …

달탐사초소형위성개발동향

심은섭 - 항공우주산업기술동향, 2017 - dbpia.co.kr
미국 우주발사시스템 (SLS) 의 첫 시험비행인 EM-1 에 탑재되는 달탐사 초소형위성들에 대해
기술하였다. SLS 는 2019 년에 주 탑재체로 오리온 우주선을, 그리고 혁신적인 아이디어를 …