A comparison study of mass-area ratio for large size x-ray telescope optics in pore and very thin glass sheets configurations

2006 ◽  
Author(s):  
S. Basso
2019 ◽  
Vol 40 (3) ◽  
Author(s):  
Vinita Navalkar ◽  
Kulinder PAL Singh ◽  
Mehernosh Press

2014 ◽  
Author(s):  
Stefano Basso ◽  
Enrico Buratti ◽  
Marta Civitani ◽  
Giovanni Pareschi ◽  
Bianca Salmaso ◽  
...  
Keyword(s):  

2021 ◽  
pp. 095605992110640
Author(s):  
Hemant Arora ◽  
Rutvik Dangarwala ◽  
Sudipto Mukherjee ◽  
Bhavdeep Singh Munjal

Space exploration arises the demand for launching large size structures to satisfy the need of high bandwidth telecommunication, earth observation and deep space interplanetary missions. Launching of these monolithic structures of sizes 3 m or more are not feasible due to limited launch fairing space of state-of-the-art launch vehicles. Therefore, the development of innovative deployment mechanisms is need of the hour. Deployment process of space borne deployable systems is the process of transition from mechanism to structure which is one of the unreliable stage due to existence of many conventional rotary joints which causes loss of energy due to backlash, friction and misalignment. An investigation study is presented in this paper for churning out a solution of flexible hinges using tape springs in state-of-the-art space deployable configurations which eliminates the factors causing loss of energy. Analytical and experimental methods are evaluated for investigating the bending behaviour of tape flexures. Tape flexures demonstrate to be a suitable candidate for compliant deployable configuration. The proposed configuration with combination of two tape flexures mounted in such a way that concave curve of each tape faces each other are structurally analysed for desired rotation angle. A comparison study is carried out for various material options of single and double layered tape flexures proposed for a flexure hinge. Practical feasibility of the proposed configuration is also demonstrated successfully on space borne deployable structures.


2019 ◽  
Vol 48 (2) ◽  
pp. 218001
Author(s):  
沈正祥 Shen Zhengxiang ◽  
张 璟 Zhang Jing ◽  
余 俊 Yu Jun ◽  
王晓强 Wang Xiaoqiang ◽  
卫俊杰 Wei Junjie ◽  
...  
Keyword(s):  

2008 ◽  
Vol 8 (5) ◽  
pp. 187S-188S
Author(s):  
Huilin Yang ◽  
Jin-Hui Shi ◽  
Jiayong Liu ◽  
Ashok Biyani ◽  
Steven Ericksen ◽  
...  

2006 ◽  
Vol 2 (S237) ◽  
pp. 421-421
Author(s):  
K. Hamaguchi ◽  
R. Petre ◽  

AbstractThe Carina Nebula possesses the brightest soft diffuse X-ray emission among the Galactic giant HII regions, but the origin has not been known yet. The XIS1 back-illuminated CCD camera onboard the Suzaku X-ray observatory has the best spectral resolution for extended soft sources so far, and is therefore capable of measuring these key emission lines in the soft diffuse plasma. Suzaku observed the Carina nebula on 2005 Aug. 29. The XIS1 spectra of the Carina nebula clearly showed spatial variations in emission line strengths. In the south, the spectrum showed strong L-shell lines of iron ions and K-shell lines of silicon ions, while in the north these lines were much weaker. Fitting the spectra with an absorbed thin-thermal plasma model with kT ~ 0.2, 0.6 keV and NH ~ −2 × 1021 cm−2 showed that the silicon and iron abundance is about 2–3 times higher in the south than in the north. Because of its large size (~40 pc), the diffuse emission in the Carina nebula might have been produced by an old supernova, or a super shell produced by multiple supernovae.


2015 ◽  
Author(s):  
C. Pelliciari ◽  
D. Spiga ◽  
E. Bonnini ◽  
E. Buffagni ◽  
C. Ferrari ◽  
...  
Keyword(s):  
X Ray ◽  

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