Ss5002 Principles Of Strength Training

[Filomeno Robles]

Thisdepartment offers courses related to the aerospace vehicle design studies especially the satellite engineering and the application of satellite for remote sensing and communication and navigation systems.

The CE103 Thermal Process Control Apparatus is one of a unique range of products designed especially for the theoretical study and practical investigation of basic and advanced control engineering principles. This includes the analysis of static and dynamic systems using analogue and or digital techniques.

The CE103 relates specially to heat and heat transfer control problems as thet would typically occur in process control industries. It may also, however be used as a practical introduction to the design, operation and application of control systems in general.

The flexible design of the equipment enables many other analysis and control exercises to be developed by the user to suit his local requirements. This includes extended or advanced control experiments. The equipment is also ideal for the student project work.

EyasSat is a nano-sat demonstrator suitable for use in the lab environment for a teaching and learning experience. It basically demonstrates the functionality of a typical satellite system built up from modules representing subsystems. Starting from the bottom, we currently have the EyasSat stack configured as follows:

Fans are mechanical instruments that allow to move great gas flows as a result of the pressure increase generated. There are two basic types of air moving devices : the centrifugal fan or blower , and the axial flow fan. Generally, centrifugal fans are more suitable for lower flows at high pressures than their axial counterparts.

The centrifugal fan is a radial flow machine that produces the necessary pressure to move gas by the centrifugal force built up inside the fan casing. The gas comes out in a radial way in relation to the shaft of the fan.

The unit has a heat source, in the form of a black body radiator, and a thermopile that measures the intensity of the radiation. It also has a light source, a luxmeter to measure illuminance, and thermocouples to measure temperatures.

The Main purpose of this project is to apply the concept of spacecraft design and to get experience in practical construction of the design through this work, the design of MAEU 001 Can Satellite. The minimal volume of the Can Sat will be fit all of the subsystems including power, sensors and communication systems. The structural subsystem of the Can Sat will provide all components to have more enough space. Communication and Data Handling system in Can Sat have a processing unit that will handle all the real time operations of the Can Sat and provide data interfaces to all other systems. Its main purpose is transmitting housekeeping and mission data from Can Sat to ground station. In order to perform the final operation safety, the recovery system which includes a parachute giving a constant descent rate of the Can Sat , will be provided to withstand the impact load.

The main aim of the project is to initiate and promote the practical application of space systems engineering in Myanmar through designing, fabrication, construction and making test operation of a Can Satellite in student project level.

i-CanSat is an affordable educational satellite kit , designed by Prof.Hironori SAHARA of Tokyo Metropolitan University. It is designed to provide training about basic satellite engineering and technology. The miniature satellite includes all the subsystems that are similar to the real satellite. The learner can acquire basic satellite engineering using iCanSat which includes knowledge about system engineering, on-board computer (OBC) , sensors , actuators, assembly, integration and testing (AIT) and project management.

3a8082e126