The beaming of external Compton emission

We consider a relativistically moving blob consisting of an isotropic electron distribution that Compton-scatters photons from an external isotropic radiation field. We compute the resulting beaming pattern, i.e. the distribution of the scattered photons, in the blob frame as well as in the observer’s frame by using the full Klein–Nishina cross section and the exact incident photon distribution. In the Thomson regime the comparison of our approach with Dermer (1995) results in concurrent characteristics but different absolute number of the scattered photons by a factor of f_corr = 3.09. Additionally, our calculation yields a slightly lower boost factor which varies the more from the corresponding value in Dermer (1995) the higher the spectral index p of the electron distribution gets.     

China''s space policy: review and prospects

This article reviews the current status of the Chinese space programme, covering its military origins, launchers, applications satellites, manned spaceflight and exploration. It examines the growing commercialization of China's space activities and how far this is likely to be successful, especially in the light of MTCR constraints and other legal regulations. It is nonetheless concluded that commercialization, along with joint ventures with foreign companies, has been crucial to the development of China's space programme. However, the country still lacks the resources to become a first-rank space power.     

Ground based ISS payload microgravity disturbance assessments

In order to verify that the International Space Station (ISS) payload facility racks do not disturb the microgravity environment of neighboring facility racks and that the facility science operations are not compromised, a testing and analytical verification process must be followed. Currently no facility racks have taken this process from start to finish. The authors are participants in implementing this process for the NASA Glenn Research Center (GRC) Fluids and Combustion Facility (FCF). To address the testing part of the verification process, the Microgravity Emissions Laboratory (MEL) was developed at GRC. The MEL is a 6 degree of freedom inertial measurement system capable of characterizing inertial response forces (emissions) of components, sub-rack payloads, or rack-level payloads down to 10(-7) g's. The inertial force output data, generated from the steady state or transient operations of the test articles, are utilized in analytical simulations to predict the on-orbit vibratory environment at specific science or rack interface locations. Once the facility payload rack and disturbers are properly modeled an assessment can be made as to whether required microgravity levels are achieved. The modeling is utilized to develop microgravity predictions which lead to the development of microgravity sensitive ISS experiment operations once on-orbit. The on-orbit measurements will be verified by use of the NASA GRC Space Acceleration Measurement System (SAMS). The major topics to be addressed in this paper are: (1) Microgravity Requirements, (2) Microgravity Disturbers, (3) MEL Testing, (4) Disturbance Control, (5) Microgravity Control Process, and (6) On-Orbit Predictions and Verification.     

Lagrangian analysis of satellite-derived currents: Application to the North Western Mediterranean coastal dynamics

Optimal interpolation methods for improving the reconstruction of coastal dynamics from along-track satellite altimetry measurements have been recently developed over the North Western Mediterranean Sea. Maps of satellite-derived geostrophic current anomalies are generated using these methods, and added to different mean circulation fields in order to obtained absolute geostrophic currents. The resulting fields are then compared to standard AVISO products, and their accuracies are assessed with Lagrangian diagnostics. The trajectories of virtual particle clusters are simulated with a Lagrangian code either with new current fields or with the AVISO ones. The simulated trajectories are then compared to 16 in situ drifter trajectories to evaluate the performance of the different velocity fields. The comparisons show that the new current fields lead to better results than the AVISO one, especially over the shallow continental shelf of the Gulf of Lion. However, despite the use of innovative strategies, some altimetry limitations still persist in the coastal domain, where small scale processes remain sub-sampled by conventional altimetry coverage but will benefit from technological development in the near future. Some of the limitations of the Lagrangian diagnostics presently used are also analyzed, but dedicated studies will be required for future further investigations.     

A market for GMES? Results of the Graz conference

A new step in defining Global Monitoring for Environment and Security (GMES) was undertaken in April 2006 by the Austrian Presidency of the EU Council. Together with the European Commission, it organised a conference on ‘A Market for GMES in Europe and its Regions- the Graz Dialogue’. Prepared by the European Space Policy Institute (ESPI), the conference assembled experts and users of GMES, who had agreed upon specific issues for discussion. The outcomes of the workshops were then brought to the Graz conference for wider reflection and discussion and summed up in the Graz Declaration (reprinted in the documentation section of this issue), which is a strategic, economic and regional action plan for GMES for the next 10 years, later endorsed by the Competitiveness Council at the end of May. This report presents the goals and outcomes of the conference and underlines the positive impulses it gave to GMES.     

CASH 2021: commercial access and space habitation

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.     

Concerning the interpretation of the ultraviolet radiation from B stars

Measurements of the shape of the ultraviolet spectrum from B stars are compared with the theoretical spectra predicted from a homogeneous series of eight model atmospheres which are known to be close to a state of radiative equilibrium and to give a good representation of the ordinarily observed spectral region. The broad-band photometer measurements of Byram, Chubb, and Friedman in the region 1314 indicate that the stars become brighter in the ultraviolet as their temperature increases. The theoretical spectra reproduce this trend. However, the theoretical spectra are about three times as bright at 1314 relative to their brightness at 5560 as is observed.The spectral observations at 50Å resolution of Stecher and Milligan of six absorption-line stars are compared in detail with theoretical spectra. The observed shape of the spectrum is reproduced well by the models from 2600 to longer wavelengths. At wavelengths shorter than 2600 Å, the observed fluxes from B stars are less than the predicted fluxes. At 2000 the deficiency is between a factor two and a factor four. The spectrum of Canis Majoris is observed to have a different shape from that found for four other early-type stars. In the case of Canis Majoris the deficiency at 2000 is about a factor 13.The proper manner in which to compare theory and observation is discussed and some astrophysical terminology is explained. Theoretical fluxes, , are given in Table 1 for eight early B type model atmospheres at wavelengths between the Lyman limit and 6251. These fluxes have been computed without consideration of the opacity due to line blanketing. It is shown that line blanketing can probably account for the differences noted between predicted and observed ultra-violet spectra of B stars. It is not necessary at present to invoke unusual sources of opacity in the stellar atmosphere or in the space between the star and the earth in order to explain the observations. Spectra of B stars in the 2000 region at sufficient resolution to show the line spectrum would clarify the problem.     

电-热耦合对航空复合材料拉伸及疲劳性能的影响

为研究碳纤维增强树脂基复合材料(CFRP)层合板的导电性能和电-热耦合效应及其对拉伸和疲劳性能的影响,主要针对2种不同铺层的试件(单向层合板(UD)[0]8和准各向异性层合板(QI)[45/90/-45/0]s)进行导电及电-热耦合实验和通电状态下的拉伸及疲劳实验。在电-热耦合实验中分别对试件通以1~8A的直流电和交流电,测量其温度场的分布及最高温度,以确定温度对电阻的影响。依据实验现象建立了简化后的电-热耦合分析模型,并与实验结果进行对比,发现两者吻合很好。简化后的电-热耦合模型能够很好地预测试件在达到稳态平衡时的最高温度值。在通电情况下对不同初始状态时的QI试件进行拉伸和疲劳实验,通过实验发现,在疲劳加载过程中无论是通以直流电、交流电或者是改变电流强度和电流频率,对试件的疲劳寿命影响不大,没有发现明显差异,但在实验过程中试件表面的温度会随着电流强度的增加而升高。同时,在监测试件沿着纤维方向的电阻变化时发现,在一定的疲劳载荷下,随着循环次数的增加,试件的电阻会不断增加,这表明试件内部出现了损伤,累积后直至试件断裂。依据实验现象分别建立了电阻模型-1和电阻模型-2,分析计算后发现模型-1能够较好地模拟试件变形的线性阶段(εxx≤0.4%),而模型-2能较好地模拟非线性阶段直至试件断裂(εxx0.4%)。