General objects: To train scientific and technical team have the ability to acquire technology and apply research results on satellite technology.

Specific objects: By the method of simulation modeling to study some technical problems about launching small satellites into orbit and influence of launch vehicle’s kinetics on the onboard equipment

• To approach and master the scientific and technical basis of launching small satellites into orbit for the acceptance of technology.
• Create a scientific base and technical products as prerequisite for the development of space technology program of the next stage.

1. Study, design and calculate the algorithm to define design parameter, configuration, technical features, orbit, control,  dynamic system, size, weight of clusters and block the function of launch vehicle put satellite into orbit.
2. Set kinetic models up and calculate motion orbit of booster rocket; design, build software programs and device to simulate the motion of the rocket to put satellites into orbit.
3. Build principles, calculate stable orbital and closed control loop dynamic system of booster rocket in active orbit stage; design and build equipment to simulate closed control loop dynamic system of booster rocket in active orbit stage.
4. Research, calculate load, structural strength of booster rocket, build methods and a set of calculation software programs, design a booster solid rocket engine structural.
5. Research, calculate, design, manufacture and test operation of physical models of creates four degrees of freedom pendulum device to simulate influence of booster rocket kinetics on the onboard equipment (satellite’s weigh about 150kg assumption).
6. Research, calculate, design, manufacture and test operation of physical models (layout) of device control system and the thrust vector drive actuator to orbit rocket.
7. Study the effect of the structure of small satellite used to observe the Earth during low orbit (LEO) and calculate, build program and equipment to simulate the motion process of small satellite into orbit.

a) Product I: 05 products

• 01 physical models of creates four degrees of freedom pendulum device that simulate influence of booster rocket kinetics on the onboard equipment
• 01 physical models (layout) of device control system and the thrust vector drive actuator to create booster rocket’s orbit
• 01 device used to simulate the motion process of a satellite booster rocket
• 01 equipment used to simulate closed control loop dynamic system of booster rocket in active orbit stage
• 01 equipment used to simulate the motion process of small satellite into low orbit

b) Product II: 09 products

• A set of scientific document "Research, calculate, design launching algorithm of a booster rocket to put satellites into orbit"
• A set of scientific document “Set kinetic models up, calculate motion orbit and simulate the motion of the rocket to put satellites into orbit”
• A set of scientific document “Build principles, calculate stable orbital simulate closed control loop dynamic system of booster rocket in active orbit stage”
• A set of scientific document “Research, calculate load, structural strength of a satellite booster rocket”
• A set of scientific document “Research, calculate, and test operation of physical models (layout) of control device system and the thrust vector drive actuator to create a booster rocket’s orbit”
• Document of technical drawings for manufacturing the physical model of control device system and the thrust vector drive actuator to create a booster rocket’s orbit
• A set of scientific document “Research, calculate, design, manufacture and test operation of physical models of creates four degrees of freedom pendulum device to simulate influence of booster rocket kinetics on the onboard equipment”
• Document of technical drawing for manufacturing devices and creates four degrees of freedom pendulum physical model to simulate influence of booster rocket kinetics on the onboard equipment
• A set of scientific document “Build program and equipment to simulate the motion process of small satellite into orbit”

c) Product III: 05 scientific articles

• Posted 03 articles in the Proceedings of the Conference of Control Automation and Robotics, applied in defense - security and National Mechanics Conference, 4/2009;
• 02 articles in the Proceedings of "Aerospace Science and Technology Conference-2010", June 12/2010 at the Science and Technology Institute of Vietnam

d) Training results:

• Master: 01, Defended Master thesis in 2009
• Doctor: 01, Will defend PhD thesis in 2013