Mission Analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI

S Campagnola, J Hernando-Ayuso… - IEEE Aerospace and …, 2019 - ieeexplore.ieee.org
OMOTENASHE and EQUULEUS are two 6-U CubeSats by JAXA and The University of
Tokyo to be launched in 2019 onboard of NASA's Exploration Mission 1. This paper …

[PDF][PDF] EQUULEUS mission analysys: design of the science orbit phase

K Oguri, K Kakihara, S Campagnola… - … Symposium on Space …, 2017 - researchgate.net
Libration point orbits, in particular those in the Earth-Moon system, have been attracting
attention for science and future human space exploration. Exploring these orbits via micro …

Design of fuel-saving lunar captures using finite thrust and gravity-braking

S Carletta - Acta Astronautica, 2021 - Elsevier
The emergence of microsatellite missions leaving low Earth orbits to pursue the exploration
of the solar system is currently leading the development of new techniques of mission …

[PDF][PDF] EQUULEUS mission analysis: design of the transfer phase

K Oshima, S Campagnola, CH Yam, Y Kayama… - … Symposium on Space …, 2017 - issfd.org
This paper highlights the design of the transfer phase of EQUULEUS (EQUilibriUm Lunar-
Earth point 6U Spacecraft), which aims to reach and stay at the Earth-Moon L2 libration point …

Technology enabling interplanetary trajectories for nanospacecraft

S Tardivel, AT Klesh, S Campagnola - Journal of Spacecraft and …, 2018 - arc.aiaa.org
Following their success in low Earth orbit, nanospacecraft weighing less than 25 kg may
soon contribute to the exploration of the Solar System. This paper outlines the necessary …

Average daily radiation dose as a function of altitude, latitude, and shielding

S Tardivel, AT Klesh, S Campagnola - Journal of Spacecraft and …, 2017 - arc.aiaa.org
THE democratization of space exploration is manifest in the number of nanospacecraft
launched in the year 2014. Two-thirds of the 158 nanosatellites (1–25 kg) and …

[PDF][PDF] A Doctor Thesis

航法誘導制御方策の統合的最適化 - repository.dl.itc.u-tokyo.ac.jp
In deep space exploration with micro/nano-spacecraft, the relatively high cost of trajectory
correction and orbit determination is an important issue. In this study, a method is proposed …

[PDF][PDF] DEVELOPMENT AND TEST OF AN ALGORITHM FOR DETECTION AND POST-PROCESSING FOR LUMIO

A Degli Innocenti, F Topputo - politesi.polimi.it
The LUMIO mission, presented as response to the fourth edition of the SysNova competition
organized by ESA, proposes to insert a CubeSat in a halo orbit near the L2 Lagrangian …

Developement and test of an algorithm for detection and post-processing for LUMIO mission

A Degli Innocenti - 2018 - politesi.polimi.it
The LUMIO mission, presented as response to the fourth edition of the SysNova competition
organized by ESA, proposes to insert a CubeSat in a halo orbit near the L2 Lagrangian …

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 …