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Sensors and Components for Aerospace Thermal Control and Propellant Systems
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English
Abstract
Various aspects of different sensors and components, (being) developed or fine-tuned for aerospace thermal control and propellant systems, are discussed, i.e.: rotatable radial heat pipe joints, vapour quality sensors, controllable valves, condensers, flow metering assemblies and propellant gauges.
Authors
Citation
Delil, A., Pauw, A., van Put, P., and Voeten, R., "Sensors and Components for Aerospace Thermal Control and Propellant Systems," SAE Technical Paper 972478, 1997, https://doi.org/10.4271/972478.Also In
References
- Delil, A.A.M. Moveable thermal joints for deployable or steerable spacecraft radiator systems SAE 871460 , 17th Intersociety Conference on Environmental Systems Seattle, WA, USA 1987
- Moschetti, B. Amidieu, M. Tatry, B. Design and test of a space deployable radiator SAE 851364 , 15th Intersociety Conference on Environmental Systems San Francisco, CA, USA 1985
- Delil, A.A.M. Quality monitoring in two-phase systems for large spacecraft SAE 860259, 16th Intersociety Conference on Environmental Systems San Diego, CA, USA 1986
- Delil. A.A.M. A sensor for high-quality two-phase flow Proc. 16th International symposium on Space Technology and Science Sapporo Japan 1988 957 966
- Delil, A.A.M. et al. TPX: In-orbit demonstration of two-phase heat transport technology in TDP1, final report 1995
- Delil, A.A.M. et al. TPX for in-orbit demonstration of two-phase heat transport technology - Evaluation of flight & postflight experiment results SAE 95150, 25th International Conference on Environmental Systems San Diego, CA, USA 1995
- Dunbar, N.W. ATLID Laser Head Thermal Control-Design and Development of a Two-Phase Heat Transport System for Practical Application SAE 961561 , 26th International Conference on Environmental Systems Monterey, CA, USA 1996
- Delil, A.A.M. et al. High Efficiency Low Pressure Drop Two-Phase Condenser for Space SAE 961562, 26th International Conference on Environmental Systems Monterey, CA, USA 1996
- Hufenbach, B. et al. Comparative assessment of gauging systems and description of a liquid gauging concept for a spin-stabilised spacecraft 2nd European Spacecraft Propulsion Conference Noordwijk, Netherlands 1997
- Delil, A.A.M. et al. Characterisation of the dielectric properties of Mixed Oxydes of Nitrides and Mono Methyl Hydrazine 1997