DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Trojan Lander Experiments In The Solar Powered Sail Mission

Okada, T. and Bibring, J.P. and Ulamec, S. and Matsumoto, J. and Kebukawa, Y. and Aoki, J. and Yano, H. and Nakamura, R. and Mori, O. (2016) Trojan Lander Experiments In The Solar Powered Sail Mission. AOGS 13th Annual Meeting, 31. Juli - 5. August, Beijing, China.

Full text not available from this repository.


A landing experiment on a Jupiter Trojan asteroid is under study in the Solar Powered Sail (SPS) mission. The SPS is based on the advanced hybrid propulsion system using the large area thin film solar array as the space yacht (inherited from IKAROS mission) and the ion engine (inherited from Hayabusa and Hayabusa2 missions), enabling the spacecraft to visit outer solar system without using a radioactive thermoelectric generator (RTG). After more than 10 years cruise to a Trojan asteroid, the spacecraft will observe the asteroid globally from the home position to characterize it. Then a 100 kg class lander will be deployed to land on the surface. The lander has about 20 kg mission instruments. When it is landed, it looks around the surroundings with panoramic imagers to characterize the geologic context and under the body with a monitor camera whether it is properly landed and ready for sampling the surface materials. If not, the lander will relocate by hopping. The surface and subsurface materials are sampled and investigated with visible and infrared microscopes to characterize the physical properties and mineral composition of them. Part of those samples are heated so that volatiles are evaporated to conduct high resolution mass spectroscopy. Isotopic ratios of nitrogen, hydrogen, and oxygen are key information to solve the origin and evolution of the asteroid, and also the solar system, because it is essential question whether the Jupiter Trojans originated around the outer asteroid belt, or from the outer solar system region. We will present the current design of surface landing experiments and the strawman payloads.

Item URL in elib:https://elib.dlr.de/107207/
Document Type:Conference or Workshop Item (Speech)
Title:Trojan Lander Experiments In The Solar Powered Sail Mission
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Okada, T.JSPEC/JAXA, Yoshinodai, Chuo, Sagamihara, Kanagawa, JapanUNSPECIFIED
Ulamec, S.DLR-Köln, stephan.ulamec (at) dlr.deUNSPECIFIED
Matsumoto, J.University of Tokyo, JapanUNSPECIFIED
Kebukawa, Y.Yokohama National University, JapanUNSPECIFIED
Aoki, J.Osaka University, JapanUNSPECIFIED
Date:31 July 2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Trojan Lander
Event Title:AOGS 13th Annual Meeting
Event Location:Beijing, China
Event Type:international Conference
Event Dates:31. Juli - 5. August
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Science and Exploration
DLR - Research area:Raumfahrt
DLR - Program:R EW - Erforschung des Weltraums
DLR - Research theme (Project):R - Explorationsstudien
Location: Köln-Porz
Institutes and Institutions:Space Operations and Astronaut Training > User center for space experiments (MUSC)
Deposited By: Herrmann, Astrid
Deposited On:08 Nov 2016 17:37
Last Modified:08 Nov 2016 17:37

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.