Similar Items: A liquefied gas thruster for a micro satellite
- Investigation of the functioning of a liquefied-gas micro-satellite propulsion system
- Strategies for the control of a satellite with thruster misalignment
- Thermal management and control of space satellite systems and subsystems in orbit
- Development of a vacuum arc thruster for nanosatellite propulsion
- A numerical investigation of the plenum chamber aerodynamic behaviour of mechanical draught air-cooled heat exchangers
- The characterisation of magnetic couplings and the development of a thruster module for an ROV
Author: Dobson, R. T.
- A liquefied gas thruster for a micro satellite
- Sustainable cooling alternatives for buildings
- Simulation and control implications of a high-temperature modular reactor (HTMR) cogeneration plant
- Experimental evaluation of a low temperature and low pressure turbine
- Indirect measurement of reactor fuel temperature
- Transient simulation of a lithium bromide-water vapour absorption refrigeration system