On-orbit Research and Validation on the Lifetime Capability of Propulsion System
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-3387-5_78
Reference15 articles.
1. Hinckel, J.N., Trava-Airoldi, V.J., Corat, E.J., et al.: Propulsion subsystem component development program for the MECB RSS satellite. In: 27th AIAA/SAE/ASME/ASEE Joint Propulsion Conference, Sacramento (1991)
2. Salim, A.A.: In-orbit performance of lockheed Martin’s electrical power subsystem for A2100 communication satellites. In: 35th Intersociety Energy Conversion Engineering Conference and Exhibit,Las Vegas (2000)
3. Kammerer, H., Hughes, J., Gribben, E.: Analytical and material advances in contoured metal diaghragms for positive expulsion tanks. In: 31st AIAA/SAE/ASME/ASEE Joint Propulsion Conference and Exhibit, San Diego (1995)
4. Cho, Y.H., Jae, H.Y., Kyun, H.L., et al.: Sensitivity analyses of satellite propulsion components with their thermal modelling. Adv. Space Res. 47, 466–479 (2011)
5. Weislogel, M.M., Sala, M.A., Collicott, S.H.: Analysis of tank PMD rewetting following thrust resettling. In: 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV (2002)
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