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1.
Victor Parque Wataru Suzaki Satoshi Miura Ayako Torisaka Tomoyuki Miyashita Michihiro Natori 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2589-2612
Elucidating versatile configurations of spiral folding, and investigating the deployment performance is of relevant interest to extend the applicability of deployable membranes towards large-scale and functional configurations.In this paper we propose new schemes to package flat and curved membranes of finite thickness by using multiple spirals, whose governing equations render folding lines by juxtaposing spirals and by accommodating membrane thickness. Our experiments using a set of topologically distinct flat and curved membranes deployed by tensile forces applied in the radial and circumferential directions have shown that (1) the multi-spiral approach with prismatic folding lines offered the improved deployment performance, and (2) the deployment of curved surfaces progresses rapidly within a finite load domain. Furthermore, we confirmed the high efficiency of membranes folded by multi-spiral patterns.From viewpoints of configuration and deployment performance, the multi-spiral approach is potential to extend the versatility and maneuverability of spiral folding mechanisms. 相似文献
2.
Previous calculations of the accumulation of small (∼10 km) planetesimals at ∼1 AU to form Mars-sized bodies assumed that
the initial assemblage of planetesimals were all present at the outset. This is an obviously reasonable assumption in systems
in which the time scale for growth time of ∼1026 g planetary bodies is long compared to estimates of the evolutionary time scale of a protosolar disk, as was the case in
the pioneering work of Safronov (1969). It is now found that as a result of the preplanetary assemblage being unstable with
respect to the runaway growth of the largest bodies, this is unlikely to be the case. The more realistic alternative of adding
the initial planetesimals on a ∼105 year time scale is considered here, as well as the consequences of the initial planetesimals being considerably smaller than
those assumed previously. It is found that although the time scale for runaway growth is now actually controlled by the availability
of planetesimals, for planetesimal production time scales of ∼105 yrs, the final consequences are very similar. These calculations do show, however, that as a consequence of continuous infall
during the runaway growth process, the late initial planetesimals are likely to be catastrophically disrupted by mutual collisions.
For this reason, a more detailed treatment of the growth of planetesimals into planetary embryos will require a better understanding
of the difficult problem of formation of the initial planetesimals themselves.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献
3.
Junichi Yamazaki Seiji Mitsuhashi Masahito Yamauchi Junichi Tachino Rie Honda Motomaro Shirao Kazuo Tanimoto Hiroyuki Tanaka Nobuaki Harajima Asako Omori Satoshi Yahagi Shigehiro Kanayama Yuichi Iijima Hisashi Ohtake 《Space Science Reviews》2010,154(1-4):21-56
The High-Definition television (HDTV) system onboard the Japanese lunar explorer Kaguya (SELENE) consists of a telephotographic camera and a wide-angle camera that each have 2.2 M-pixel IT-CCDs (interline transfer charge-coupled devices) and LSIs (large-scale integrated circuits) of the several-million-gates class. One minute-long motion pictures acquired by the HDTV system at 30 fps (frames per second) are recorded in a 1 GB semiconductor memory after compression, and then transmitted to a ground station. In the development of the space-going HDTV system, a commercial ground-model HDTV system was extensively modified and evaluated for its suitability to withstand the harsh environment of space through environmental tests. The HDTV acquired a total of 6.3 TB of movies and still images of the Earth and the Moon over the mission period that started on September 29, 2007, and ended on June 11, 2009. Footage of an “Earth-rise” and an “Earth-set” on the lunar horizon were captured for the first time by the HDTV system. During a lunar eclipse, images of the Earth’s “diamond ring” were acquired for the first time. The CCDs and the instruments used in the system remained in good working order throughout the mission period, despite the harsh space environment, which suggests a potential new approach to the development of instruments for use in space. 相似文献
4.
Morikawa E. Miura R. Matsumoto Y. Kimura K. Arakaki Y. Ohmori S. Wakana H. 《IEEE transactions on aerospace and electronic systems》1995,31(2):784-794
We developed two types of hybrid terminals that can provide both satellite communication and position determination services in one system. One terminal uses the single channel per carrier (SCPC) technique and the other uses the spread spectrum (SS) technique. To evaluate the performance of the two systems, we carried out experiments in Japan and in the Pacific Ocean using two geostationary satellites, ETS-V (150°E) and Inmarsat (180°E). The ranging accuracy between the mobile terminals and the base station via the satellites was found to be about 200 m using the SCPC system and about 10 m using the SS system. The measured positioning accuracy was about 1 km in the SCPC system and about 600 m in the SS system when experiments were carried out near Japan. The experimental results show that the positioning errors were mainly caused by the orbital determination errors of the two satellites. Presented here are the configurations and features of the SCPC and SS terminals, the experimental system, and the experimental results 相似文献
5.
Chikako Takahashi Makoto Suzuki Chihiro Mitsuda Satoshi Ochiai Naohiro Manago Hiroo Hayashi Yoshitaka Iwata Koji Imai Takuki Sano Masahiro Takayanagi Masato Shiotani 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
We estimate the capability of ozone (O3) retrieval with the Superconducting Submillimeter-Wave Limb-Emission Sounder (SMILES) instrument attached to the Exposed Facility of the Japanese Experiment Module (JEM) on the International Space Station (ISS). SMILES carries a 4-K mechanical refrigerator to cool superconducting devices in space. Since SMILES has high sensitivity thanks to the superconducting receiver, it is expected that SMILES has ability to retrieve O3 profiles more precisely than the previous millimeter–submillimeter limb measurements from satellites. 相似文献
6.
Design concept of Quasi Zenith Satellite System 总被引:3,自引:0,他引:3
Noriyasu Inaba Akihiro Matsumoto Hidemi Hase Satoshi Kogure Mikio Sawabe Koji Terada 《Acta Astronautica》2009,65(7-8):1068-1075
The Quasi Zenith Satellite System, a Japanese satellite navigation system, is under development. The system broadcasts GPS-interoperable and augmentation signals as well as original Japanese signals from an inclined, elliptical geosynchronous orbit. Using this system, users around Japan and Oceania can use seamless positioning, navigation, and timing services, even in urban canyons and mountainous areas. A government policy supports the project to promote the use of geographical spatial information linked to satellite-based navigation for a wealthy and secure life in accordance with the rapid increase of satellite navigation users nationwide. To support that policy, JAXA is in charge of developing the first stage of QZSS in collaboration with related ministries and national institutes. Attention is devoted to making the system reliable and economical using legacy Japanese GEO satellite system technologies, not only satellite technology, but also ground systems and operations technologies. 相似文献
7.
Aldrin A Amara A Aris L Baierl N Beatty P Beaulieu C Behnke T Castegini R Chauhan A Cojanis P Dayawansa P Diop M Eito K Engle S Feretti S Gassama H Genova B Goulding C Janjua J Jansaeng T Jousset F Kopik A Laurin C Leggatt J Li H Mezzadri M Miura A Nolet S Ogami S Patry J Patten L Payerne C Peer G Prampolini M Rheaume C Saary J Spehar D Sufi A Sun B Thompson JB Thomson W Trautner R Tursunmuratov M Venet V Wilems E Wilson H Wittwer K Wokke F Wu Y Zhou S Zilioli I 《Acta Astronautica》2002,51(1-9):637-646
Issues about commercialization of space have been a growing concern in the past decade for the space community. This paper focuses on the work from a team of 51 students attending the Summer Session Program of the International Space University in Bremen, Germany. CASH 2021 (Commercial Access and Space Habitation) documents a plan that identifies commercial opportunities for space utilization that will extend human presence in space, and will chart the way forward for the next 20 years. The group selected four commercial sectors that show the most promise for the future: tourism, entertainment, space system service, assembly and debris removal, and research and development/production. The content of this document presents the results of their research. Historical activities in each of the commercial sectors are reviewed along with the current market situation. To provide a coherent background for future commercialization possibilities a scenario has been developed. This scenario includes a postulated upon ideal future and includes social, political and economic factors that may affect the space industry over the timeline of the study. The study also presents a roadmap, within the limited optimistic scenario developed, for the successful commercialization of space leading to future human presence in space. A broad range of commercially viable opportunities, not only within the current limits of the International Space Station, but also among the many new developments that are expected by 2021 are discussed. 相似文献
8.
Akira Miura 《Space Science Reviews》2001,95(1-2):387-398
After introducing a mathematical definition of the tail-like equilibrium and the dipole-like equilibrium in the magnetosphere, it is shown by using physical intuition based on the Energy Principle that the incompressible assumption for the ballooning instability is more valid for the tail-like configuration when the unstable ballooning mode is strongly localized near the equator. Therefore, before the substorm onset, the near-Earth plasma sheet becomes more tail-like and more likely to be subject to the ballooning instability without the stabilizing influence of the compressibility, when the critical plasma due to the stabilizing tension force is exceeded. The onset of the ballooning instability in the near-Earth plasma sheet seems promisingly relevant to the substorm onset phenomena. Also, the effect of the stochastic plasma dynamics on the ballooning and interchange instabilities is clearly shown. 相似文献
9.
Satoshi Miura Kazuki Saito Ayako Torisaka Victor Parque Tomoyuki Miyashita 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(9):2706-2715
A shape of the satellite’s solar sail membrane is essential for unloading angular momentum in the three-axis stabilized attitude control system because the three-dimensional solar sail can receive solar radiation pressure from arbitrary directions. In this paper, the objective is the shape optimization of a three-dimensional membrane-structured solar sail using the angular momentum unloading strategy. We modelled and simulated the solar radiation pressure torque, for unloading angular momentum. Using the simulation system, since the unloading angular momentum rate is maximized, the shape of the three-dimensional solar sail was optimized using a Genetic algorithm and Sequential Quadratic Programming. The unloading velocity in the optimized shaped solar sail was greatly improved with respect to a conventional flat or pyramid solar sail. 相似文献
10.
H. Saito Y. Masumoto T. Mizuno A. Miura M. Hashimoto H. Ogawa S. Tachikawa T. Oshima A. Choki H. Fukuda M. Hirahara S. Okano 《Acta Astronautica》2001,48(5-12)
This paper describes outline of the piggy-back satellite “INDEX” for demonstration of advanced satellite technologies as well as for observation of fine structure of aurora. Aurora observation will be carried out by three cameras(MAC) with a monochromatic UV filter. Electron and ion spectrum analyzer (ESA/ISA) will measure the particle phenomena together with the aurora imaging. INDEX satellite will be launched in 2002 by Japanese H2-A. The satellite is mainly controlled by the high-speed, fault-tolerant on-board RICS processor (three-voting system of SH-3). The attitude control is a compact system of three-axis stabilization. Although the size of INDEX is small (50Kg class), several newly-developed technologies are applied to the satellite system, including silicon-on-insulator devices, variable emittance radiator, solar-concentrated paddles, lithium-ion battery, and GPS receiver with all-sky antenna-coverage. 相似文献