PPT-ROCKET

R O bust C oncept and K nowledge E xtraction from T ext Shi Yu Glenn Fung August 2016 SDA Outlook Brief Intro to AmFam and SDA Background Motivation Potential B usiness Value. rocket rocket Rocket M is a rugged, hi-power, very linear performance. It features incredible range speed (150+Mbps real TCP/IP).Rocket M combines the “brains” in one choice of AirMax BaseSt Launch Vehicle. Launch . Vehicle Summary.  . The length of the rocked is 114.500 inches, and the mass is 373.66 ounces..  .  . We have a dual Deployment Recovery System with a 24 inch drogue parachute and a 72 inch main parachute. The drogue is a Fruity Chutes Classic with high strength webbing and the main parachute is a Fruity Chutes Iris Ultra Parachute.. By. Mr. Lewis. Rocket History. . 1. st. solid fuel rockets were made by the Chinese before the 1200s. . - made with gunpowder. - brought to Europe during the 1200’s. - used for warfare, but were not accurate. An exact quantity of nitrogen gas must be produced in an instant in order for an airbag to work properly.. The reaction involved is the decomposition of Sodium Nitride. Assume . that 65.1 L of N. 2. High Powered Rocketry Club. 2015-2016 . PDR . Presentation. 1. PDR Overview . 2. Vehicle. Design. Recovery. Mission Performance. Interfaces and Integration. AGSE. Design. Arm . Rocket Erection . Igniter Insertion. Kerosene and O. 2. Must be pumped very fast and at a high pressure.. Pump turbines spin at 35,000 rpm, which is twice as fast as a jet engine.. Kerosene and O. 2. Temperature. The temp inside the combustion chamber has to be extreme in order to achieve maximum thrust.. *Black Hole Performance May Vary. Rocket engines are, on the one hand, so simple that you can build and fly your own model rockets very easily. On the other hand, rocket engines (and their fuel systems) are so complicated that only three countries have actually ever put people in orbit. We will look at rocket engines to understand how they work, as well as to understand some of the complexity surrounding them.. Background for Rocket Memo. 1. Goals. The goals . of this . project:. I. ntroduce . class members . to . the design, analysis, and test process. . Develop team skills. Reinforce or preview course content. © . Microsoft Encarta. Rocket Propulsion. F. . t. =. m. . v. So:. F = engine thrust. . t = time to burn fuel. m = mass of fuel burned. . v = exhaust gas velocity. Rocket Propulsion. F. . The newest restaurant in Heathbrook republic . The food is so good you would want it for breakfast lunch and dinner.. With an all you can eat salad bar and free sauces. . You can even have free bread sticks. *Black Hole Performance May Vary. Rocket engines are, on the one hand, so simple that you can build and fly your own model rockets very easily. On the other hand, rocket engines (and their fuel systems) are so complicated that only three countries have actually ever put people in orbit. We will look at rocket engines to understand how they work, as well as to understand some of the complexity surrounding them.. www.sciencebuddies.org. Balloon Rockets. Newton’s third law: for every action, there is an equal and opposite reaction. Air is pushed out the back of the balloon. The balloon is pushed forward. Straw. Polar . Night Nitric Oxide . (. PolarNOx. ) Mission. : . The processes associated with aurora create . nitric oxide, but in the polar night there is no significant process for destroying the nitric oxide. We believe it builds up to large concentrations. The purpose of our rocket is to measure the abundance and altitude of peak abundance for the nitric oxide. Harding . University Flying Bison 2010 USLI Team. Team Official. Project Progress Manager. Safety Officer. Edmond Wilson. Cortney, Mgr.. Edmond Wilson. Airframe. Motor. Science Payload. Avionics. Launch Operations.