Subjects -> AERONAUTICS AND SPACE FLIGHT (Total: 124 journals)
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- Inflatable Lunar Habitat: Mars Mission
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Authors: Sukriti Dogra, Shruti H. Kapur, Mridula Sharma Pages: 1 - 4 Abstract: The environment of Earth is being harmed, and the planet is degrading due to the exponential population growth and resource depletion. A collision with an asteroid could completely destroy the Earth thus causing extinction of the entire human species, so a settlement at a different planet could save the extinction of human race. A civilization on another planet could prevent the extinction of the human race since an asteroid collision could entirely destroy Earth and wipe out the whole human species. Research in several branches of science and engineering is being done in order to explore and colonise the universe, which is now possible thanks to modern technology. Organizations like “Space X” are planning to take people to Mars in the near future (2026–2030). For the people who will be living and working there, this creates a significant demand for livable spaces and shelters. The future of construction on Mars offers tremendous opportunity for research and creative suggestions on how to establish a colony there. The objective of the current study is to examine the possibilities and ideas for life on Mars. PubDate: 2022-12-17 Issue No: Vol. 11, No. 3 (2022)
- An Approach for two Line Element Generation of Resident Space Objects from
Radar/Optical Telescope Observations-
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Authors: Anita Kumari, D. Rajarajan, Bidyut B. Gogoi, Nirmala S, A Kartik Pages: 5 - 14 Abstract: For safeguarding the space assets, it is imperative on our part to know about the location of Resident Space Objects (RSO) in space. Two-Line Element Sets (TLEs) are indispensable in the assessment of a RSO’s orbit in space and thereby it helps in overcoming threats to space assets by appropriate action. In the present work, we have proposed an approach to generate TLE of all the RSOs using long arc/short arc estimated orbit from RADAR/Optical Telescope based multi-arc, multi stations observations from Indian stations. This estimated orbit is used as initial guess for TLE for refined estimation. Results are compared with the estimated precise orbit which demonstrates that the proposed methodology generate fair TLE that can be consistent with the available ones and hence this TLE generation methodology can serve as an alternative tool for generating TLEs of RSOs in space. PubDate: 2022-12-14 Issue No: Vol. 11, No. 3 (2022)
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