排序方式: 共有60条查询结果,搜索用时 0 毫秒
31.
F Yatagai T Takahashi S Kitayama 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1983,3(8):65-69
W-reactivation (WR) and W-mutagenesis (WM) were observed after irradiation of phage chi X 174 with He and N ions (4.6 MeV/amu). The relative amount of phage RFI DNA (RARFI) extracted from the infected cells was determined by agarose gel electrophoresis. It was found that RARFI was increased by prior UV-irradiation of host cells and this increase corresponded to the efficiency of WR. 相似文献
32.
H. Takahashi S. Costa Y. Otsuka K. Shiokawa J.F.G. Monico E. Paula P. Nogueira C.M. Denardini F. Becker-Guedes C.M. Wrasse A.S. Ivo V.C.F. Gomes W. Gargarela Jr. N. Sant’Anna R. Gatto 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The total electron content (TEC) in the equatorial and low-latitude ionosphere over Brazil was monitored in two dimensions by using 2011 data from the ground-based global navigation satellite system (GNSS) receiver network operated by the Brazilian Institute for Geography and Statistics. It was possible to monitor the spatial and temporal variations in TEC over Brazil continuously during both day and night with a temporal interval of 10 min and a spatial resolution of about 400 km. The daytime equatorial ionization anomaly (EIA) and post-sunset plasma enhancement (PS-EIA) were monitored over an area corresponding to a longitudinal extension of 4000 km in South America. Considerable day-to-day variation was observed in EIA and PS-EIA. A large latitudinal and longitudinal gradient of TEC indicated a significant ionospheric range error in application of the GNSS positioning system. Large-scale plasma bubbles after sunset were also mapped over a wide range. Depletions with longitudinally separated by more than 800 km were observed. They were extended by more than 2000 km along the magnetic field lines and drifted eastward. It is expected that 2-dimensional TEC mapping can serve as a useful tool for diagnosing ionospheric weather, such as temporal and spatial variation in the equatorial plasma trough and crest, and particularly for monitoring the dynamics of plasma bubbles. 相似文献
33.
Jonathan F.C. Herman Aline K. Zimmer Johannes P.J. Reijneveld Kathryn L. Dunlop Yu Takahashi Simon Tardivel Daniel J. Scheeres 《Acta Astronautica》2014
This paper presents a mission analysis comparison of human missions to asteroids using two distinct architectures. The objective is to determine if either architecture can reduce launch mass with respect to the other, while not sacrificing other performance metrics such as mission duration. One architecture relies on chemical propulsion, the traditional workhorse of space exploration. The second combines chemical and electric propulsion into a hybrid architecture that attempts to utilize the strengths of each, namely the short flight times of chemical propulsion and the propellant efficiency of electric propulsion. The architectures are thoroughly detailed, and accessibility of the known asteroid population is determined for both. The most accessible asteroids are discussed in detail. Aspects such as mission abort scenarios and vehicle reusability are also discussed. Ultimately, it is determined that launch mass can be greatly reduced with the hybrid architecture, without a notable increase in mission duration. This demonstrates that significant performance improvements can be introduced to the next step of human space exploration with realistic electric propulsion system capabilities. This leads to immediate cost savings for human exploration and simultaneously opens a path of technology development that leads to technologies enabling access to even further destinations in the future. 相似文献
34.
Abstract This paper discusses embedding in a two-dimensional plane a symbolic representation for spatial data using the simple objects, points (P), lines (L), circuits (C), and areas (A). We have proposed PLCA as a new framework for a qualitative spatial reasoning. In a PLCA expression, the entire figure is represented in a form in which all the objects are related. We investigate the conditions for two-dimensional realizability of a PLCA expression, and derive the relation that the numbers of objects in a PLCA expression should have. In this process, we use the well-known Euler's formula. We also give an algorithm for drawing the figure of the PLCA expression that satisfies this condition in a two-dimensional plane and prove its correctness. The algorithm generates a quantitative expression from qualitative expression. 相似文献
35.
Koji Imai Makoto Suzuki Chikako Takahashi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
We present a calculation of the accuracy and speed of the Voigt function of various algorithms (Armstrong (1967), Hui et al. (1978), Humlicek (1982) and improved version of Kuntz (1997) developed in this study) for making the faster and higher accuracy forward model required for the Superconducting Submillimeter-Wave Limb-Emission Sounder (SMILES) Level 2 (L2) data processing system. 相似文献
36.
T Ohnishi K Tsuji T Ohmura H Matsumoto X Wang A Takahashi S Nagaoka A Takabayashi A Takahahsi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1998,21(8-9):1077-1080
Using Western blot analysis, here, we report the levels of HSP72 in several organs from goldfish which were taken into space on the NASA space shuttle. A remarkable accumulation of HSP72 was detected in muscle and spleen of those fish taken into space as compared with controls. These results suggested that the HSP72 induction is a kind of stress response at the molecular level introduced by the space environment consisting of microgravity and/or cosmic radiation as stressors. 相似文献
37.
Philippe Caisso Alain Souchier Christophe Rothmund Patrick Alliot Christophe Bonhomme Walter Zinner Randy Parsley Todd Neill Scott Forde Robert Starke William Wang Mamoru Takahashi Masahiro Atsumi Dominique Valentian 《Acta Astronautica》2009,65(11-12):1723-1737
Liquid-propellant rocket engines are widely used all over the world, thanks to their high performances, in particular high thrust-to-weight ratio. The present paper presents a general panorama of liquid propulsion as a contribution of the IAF Advanced Propulsion Prospective Group.After a brief history of its past development in the different parts of the world, the current status of liquid propulsion, the currently observed trends, the possible areas of future improvement and a summarized road map of future developments are presented. The road map includes a summary of the liquid propulsion status presented in the “Year in review 2007” of Aerospace America.Although liquid propulsion is often seen as a mature technology with few areas of potential improvement, the requirements of an active commercial market and a renewed interest for space exploration has led to the development of a family of new engines, with more design margins, simpler to use and to produce associated with a wide variety of thrust and life requirements. 相似文献
38.
Scott D. Barthelmy Louis M. Barbier Jay R. Cummings Ed E. Fenimore Neil Gehrels Derek Hullinger Hans A. Krimm Craig B. Markwardt David M. Palmer Ann Parsons Goro Sato Masaya Suzuki Tadayuki Takahashi Makota Tashiro Jack Tueller 《Space Science Reviews》2005,120(3-4):143-164
he burst alert telescope (BAT) is one of three instruments on the
Swift MIDEX spacecraft to study gamma-ray bursts (GRBs). The BAT first detects the GRB and localizes the burst direction to an
accuracy of 1–4 arcmin within 20 s after the start of the event. The GRB trigger initiates an autonomous spacecraft slew to
point the two narrow field-of-view (FOV) instruments at the burst location within 20–70 s so to make follow-up X-ray and optical
observations. The BAT is a wide-FOV, coded-aperture instrument with a CdZnTe detector plane. The detector plane is composed
of 32,768 pieces of CdZnTe (4×4×2 mm), and the coded-aperture mask is composed of ∼52,000 pieces of lead (5×5×1 mm) with a
1-m separation between mask and detector plane. The BAT operates over the 15–150 keV energy range with ∼7 keV resolution,
a sensitivity of ∼10−8 erg s−1 cm−2, and a 1.4 sr (half-coded) FOV. We expect to detect > 100 GRBs/year for a 2-year mission. The BAT also performs an all-sky
hard X-ray survey with a sensitivity of ∼2 m Crab (systematic limit) and it serves as a hard X-ray transient monitor. 相似文献
39.
A. Takahashi H. Suzuki K. Omori M. Seki T. Hashizume T. Shimazu N. Ishioka T. Ohnishi 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The 53 kDa tumor suppressor protein p53 is generally thought to contribute to the genetic stability of cells and to protect cells from DNA damage through the activity of p53-centered signal transduction pathways. To clarify the effect of space radiation on the expression of p53-dependent regulated genes, gene expression profiles were compared between two human cultured lymphoblastoid cell lines: one line (TSCE5) has a wild-type p53 gene status, and the other line (WTK1) has a mutated p53 gene status. Frozen human lymphoblastoid cells were stored in a freezer in the International Space Station (ISS) for 133 days. Gene expression was analyzed using DNA chips after culturing the space samples for 6 h on the ground after their return from space. Ground control samples were also cultured for 6 h after being stored in a frozen state on the ground for the same time period that the frozen cells were in space. p53-Dependent gene expression was calculated from the ratio of the gene expression values in wild-type p53 cells and in mutated p53 cells. The expression of 50 p53-dependent genes was up-regulated, and the expression of 94 p53-dependent genes was down-regulated after spaceflight. These expression data identified genes which could be useful in advancing studies in basic space radiation biology. The biological meaning of these results is discussed from the aspect of gene functions in the up- and down-regulated genes after exposure to low doses of space radiation. 相似文献
40.
Masaki Matsushima Hideo Tsunakawa Yu-ichi Iijima Satoru Nakazawa Ayako Matsuoka Shingo Ikegami Tomoaki Ishikawa Hidetoshi Shibuya Hisayoshi Shimizu Futoshi Takahashi 《Space Science Reviews》2010,154(1-4):253-264
To achieve the scientific objectives related to the lunar magnetic field measurements in a polar orbit at an altitude of 100 km, strict electromagnetic compatibility (EMC) requirements were applied to all components and subsystems of the SELENE (Kaguya) spacecraft. The magnetic cleanliness program was defined as one of the EMC control procedures, and magnetic tests were carried out for most of the engineering and flight models. The EMC performance of all components was systematically controlled and examined through a series of EMC tests. As a result, the Kaguya spacecraft was made to be very clean, magnetically. Hence reliable scientific data related to the magnetic field around the Moon were obtained by the LMAG (Lunar MAGnetometer) and the PACE (Plasma energy Angle and Composition Experiment) onboard the Kaguya spacecraft. These data have been available for lunar science use since November 2009. 相似文献