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排序方式: 共有171条查询结果,搜索用时 62 毫秒
101.
Andreas Rittweger Werner Beuchel Martin G. Andersen Jochen Albus 《Acta Astronautica》2005,57(12):877-886
The dynamic qualification of the new cryogenic upper stage ESC-A of the ARIANE 5 is supported by several tests in order to verify the assumptions and the modeling approach made at the beginning of the development. The stage contains a large amount of equipment such as propellant lines, acceleration rockets, batteries, fluid control equipment etc. For the low frequency domain the verification of the equipment responses in the integrated state was done by a sine vibration test, excited to levels representing the predicted flight loads including a qualification factor. Acoustic tests with the upper stage were performed to verify the random vibration responses in the frequency range up to 2000 Hz. To verify the shock response level induced by stage separation (pyro-shock) a stage separation test was performed. The paper concentrates on the experience made with the modal identification and sine vibration test of the stage. For the sine vibration test an electro-dynamic multi-shaker table was used. It was able to produce the required input precisely up to as specified, not an easy task for a test set-up of 20 tons weight. The paper presents the approach of how the dynamic qualification was reached successfully and highlights the experience accomplished. 相似文献
102.
A general set of equations is developed from which the effects of initial condition perturbations upon weapon impact point are readily evaluated. Data are presented to illustrate the accuracy with which predictions can be made. Results obtained from the actual ballistic equations, from the time-varying perturbation equations, and from a time-invariant approximation of the perturbation equations are compared. It is shown that reasonable impact point predictive accuracy can be provited for fairly large changes in initial conditions. 相似文献
103.
A novel autonomous low-cost on-board data handling architecture for a pin-point planetary lander 总被引:1,自引:0,他引:1
Tanya Vladimirova Muhammad Fayyaz Martin N. Sweeting Valentin I. Vitanov 《Acta Astronautica》2011,68(7-8):811-829
There has been increased interest in the exploration of the Moon in recent years. Pin-point precision landing is highly desirable for future lunar missions. This paper is concerned with the design of the on-board data handling (OBDH) subsystem for the pin-point lunar lander of the Magnolia-1 project, funded by NASA. Four proposed on-board data handling architectures are outlined and compared in terms of power consumption, performance and reliability. Implementation results are presented, which are obtained from prototyping of the flight computer for the optimal OBDH architecture option on a Xilinx Virtex-5 Field Programmable Gate Array. 相似文献
104.
A.A. Gusev T. Kohno W.N. Spjeldvik I.M. Martin G.I. Pugacheva A. Turtelli Jr. 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1998,21(12):1805-1808
At the interface between the upper atmosphere and the radiation belt region, there exists a secondary radiation belt consisting mainly of energetic ions that have become neutralized in the ring current and the main radiation belt and then re-ionized by collisions in the inner exosphere. The time history of the proton fluxes in the 0.64 – 35 MeV energy range was traced in the equatorial region beneath the main radiation belts during the three year period from 21 February 1984 to 26 March 1987 using data obtained with the HEP experiment on board the Japanese OHZORA satellite. During most of this period a fairly small proton flux of −1.2 cm−2 s−1 sr−1 was detected on geomagnetic field lines in the range 1.05 < L < 1.15. We report a few surprisingly deep and rapid flux decreases (flux reduction by typically two orders of magnitude). These flux decreases were also long in duration (lasting up to three months). We also registered abrupt flux increases where the magnitude of the proton flux enhancements could reach three orders of magnitude with an enhancement duration of 1–3 days. Possible reasons for these unexpected phenomena are discussed. 相似文献
105.
Michael Martin 《航空制造技术》2007,(7):110-111
高效的驱动系统需要精确的位置信息.一种特殊的光栅鼓栅线制造工艺和独特的扫描原理使海德汉新系列的角度编码器具有很高的精度. 相似文献
106.
Susan Jason Alex da Silva Curiel Doug Liddle Francis Chizea Ugur Murat Leloglu Mustafa Helvaci Mohammed Bekhti Djouad Benachir Lee Boland Luis Gomes Martin Sweeting 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
This paper focuses on ways in which space is being used to build capacity in science and technology in order to: 相似文献
107.
Martin Friedrich Martin Fankhauser 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Neural network (NN) models for the low latitude and the polar ionosphere from the D- to the F-region were developed which are based on incoherent scatter radar data from Arecibo and EISCAT Svalbard, respectively. The various geophysical input parameters defining the NN are not only the ones that represent the time one wants to predict, but also the geophysical conditions prior to the time of the prediction. The optimum length of these preceding periods are derived for the two models are different, but a period of 60 days is a compromise acceptable for both latitudes. Furthermore from the Arecibo data time constants of electron density decay after sundown are derived which – arguably – are also relevant elsewhere, including the polar latitudes. Whereas at all altitudes the electron densities decay exponentially after sundown, below 300 km there is an additional variation with solar zenith angle. 相似文献
108.
Effects of X2-class solar flare events on ionospheric GPS-TEC and radio waves over Brazilian sector 总被引:1,自引:0,他引:1
A.J. de Abreu M. Roberto M.A. Alves J.R. Abalde P.A.B. Nogueira K. Venkatesh P.R. Fagundes R. de Jesus M. Gende I.M. Martin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(11):3586-3605
In this investigation, we present and discuss the effects of 6 X2-class solar flare events in the ionospheric F region over Brazilian sector that occurred during 2013 to 2015. For this investigation, we present the vertical total electron content (VTEC) observations from nearly 120 Global Positioning System (GPS) receivers all over the Brazilian sector for each event. Also, ionospheric sounding observations obtained in São José dos Campos (23.2°S, 45.9°W, dip latitude 17.6°S; hereafter referred to as SJC), under the southern crest of the equatorial ionospheric anomaly (EIA), Brazil, are presented. The observations show that the greatest TEC impact occurs with the EUV fluxes increases lasting for more than one hour and when the solar active region is located close to the solar disc center. We present a detailed study of the efficiency of the EUV flux with wavelengths ranging from 0.1 to 190?nm for the F region ionization. The largest increase of ΔTEC occurs below the magnetic equator line, covering mainly the central, northeast, southeast and south regions, which includes the equatorial ionospheric anomaly (EIA) region. The ionograms show partial or total fade out in the echoes traces observed causing blackouts of radio signals of up to 60?min, which can have serious consequences to technological systems of public and private agencies around Brazilian sector. This study can help to better understand the effects of solar flares in the ionospheric F region. 相似文献
109.
V D Kern F D Sack N J White K Anderson W Wells C Martin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1999,24(6):775-778
To accommodate a spaceflight experiment with moss (SPM), experiment-unique equipment (EUE) was developed by engineers at Kennedy Space Center. The hardware allows sterile culture for an extended period of time in commercial petri dishes, lateral illumination of each culture with light of a specific wavelength (660 nm; other wavelengths are possible) and a range of intensities (0.05-5 micromoles photons m-2 s-1), incubation in complete darkness, and chemical fixation to terminate the experiment under conditions of microgravity. The use of a fixative required triple containment to protect the astronaut crew. An external panel on the experiment container allowed the timing of illumination and fixation to be controlled by the crew. Light quality is provided by light emitting diodes (LEDs) that are located in the lid of the outer container, the BRIC (Biological Research In Canisters)-LED. Each canister accommodates 6 Petri Dish Fixation Units (PDFUs), and each PDFU holds one 6 cm petri dish. All components are autoclavable. LED illumination is piped through a transparent glass rod. Each PDFU contains fixative in a reservoir that is released by the depression of an actuator. This hardware performed well during its first flight, the 16-day STS-87 mission in Nov./Dec., 1997 as part of the Collaborative USA and Ukrainian Experiment (CUE). It supported vigorous and sterile moss growth, cells were maintained in position and were well-fixed, and there was a vigorous and consistent response to light. Although here used for moss, in future flight experiments this unique new hardware can be used for many types of organisms normally grown in petri dishes, with or without a requirement for illumination. 相似文献
110.
D. Lemke M. Grewing P. Preussner W. Martin D. Offermann G. Lange S. Drapatz R. Katterloher H. Denner G. Klipping F. Dahl K. Proetel 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1985,5(3):11-17
The liquid helium cooled 50 cm-IR-telescope is equipped with a 4-band-camera, a photopolarimeter, a grating spectrometer and a Michelson interferometer. These focal plane instruments allow measurements with high spectral resolution, high sensitivity and diffraction limited spatial resolution in the wavelength region 2.5 … 200 μm. - The “thermal model” phase of the project was successfully completed in 1983. This phase included the development and construction of a full size cryostat, which was thoroughly tested by an experiment simulator. Prototypes of all focal plane instruments have been developed and severral have already been tested under the expected flight conditions. - At present the “flight model” phase to be entered in 1984 is being prepared. The first Spacelab flight of the reusable IR observatory is planned for 1988. It will include measurements in astrophysics, atmospheric science and helium II physics. 相似文献