A Conjoint Analysis of Propellant Budget and Maneuver Life for a Communication Satellite

Author:

ÖZ İbrahim

Publisher

Sakarya University Journal of Computer and Information Sciences

Reference16 articles.

1. [1] R. C. Benthem, et al., “ Accuracy analysis of propellant gauging systems”, 43rd International Conference on Environmental Systems, pp. 3300, 2013.

2. [2] R. Nariyoshi, S. Chernikov, and B. S.Yendler,, “Prediction of Spacecraft Remaining Life-Challenges and Achievements”, 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, pp. 4162, 2013.

3. [3] J. W. Eun, “A Study on Fuel Estimation Algorithms for a Geostationary Communication & Broadcasting Satellite”, Journal of Astronomy and Space Sciences, 17(2), pp.249-256., 2000.

4. [4] B. S. Yendler, M. Myers, N. Chilelli, S. Chernikov, J. Wang, A. Djamshidpour, “Implementation of Thermal Gauging Method for ABS 1A (LM 3000) satellite”, 14th International Conference on Space Operations, (p. 2458)., 2016.

5. [5] B. S. Yendler, J. Molinsky, S. Chernikov, D. Guadagnoli, “Comparison of gauging methods for Orbital’s GEOStarTM 1 Satellites”, SpaceOps 2014 Conference, pp.1810, 2014.

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