'Grc nasa gov' presentation slideshows

Monte Carlo, Euler and Quaternions

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MAE 1202: AEROSPACE PRACTICUM

MAE 1202: AEROSPACE PRACTICUM. Lecture 5: Compressible and Isentropic Flow 1 February 11, 2013 Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk. READING AND HOMEWORK ASSIGNMENTS. Reading: Introduction to Flight , by John D. Anderson, Jr.

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Flight Simulators to Teach STEM

Flight Simulators to Teach STEM. Gerald E. Murray, M.A., M.Ed. murray.gerald.e@gmail.com. Gerald Murray. Elementary teacher, science presenter: CAST, NSTA Private Pilot 1000+ hours flying Single engine, Multi-engine, glider Simulator pilot Embarrassing number of hours.

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George Bucsan Marco Romero Nick Solarz Evan Molenda Peter Vardakas

Aircraft Rudder Servo. George Bucsan Marco Romero Nick Solarz Evan Molenda Peter Vardakas. Aircraft Rudder Servo Control. Rudder Basics Model Construction PID control and Tuning Simulink Wind Tunnel Testing CFD testing Conclusion. Project Goal.

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Air Flow Unlimited

Air Flow Unlimited. Group 13 Joseph Cognato Jonathan Glynn Matthew Hartman Ramon Villarreal. Intro. Airfoil structure analysis Airfoil force calculations and material selection Shape evaluation for the carts Spring selection and material choices for the carts

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States of Matter

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AeroAstro Outreach Program & Wind Tunnel Demonstration

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Microthruster Test Rig Design Review Presentation

Erik Mueller Michael White. Microthruster Test Rig Design Review Presentation . Contents. Introduction Problem Solution Sensing Frame Testing Q&A Sources. Microthrusters. Microthrusters produce <1N of thrust ( mN range) Various propulsion systems (standard, mono, ion drive).

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Liquids and Solids

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AeroAstro At MIT & Wind Tunnel Demonstration

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Rocket Construction

Rocket Construction. Ou r Goal. Some questions: What do we hope to accomplish? What specification are required to accomplish this goal? How can we design to those specifications? What elements can we change with this rocket?. Parts of a Model Rocket. Body Tube Cylindrical cardboard tube

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Arbitrary Payload Cost Optimization to LLO

Arbitrary Payload Cost Optimization to LLO. Tasks: Payload Cost / Mass Optimization (Launch to LLO) Disprove Momentum Transfer Alternative Disprove Spinning Mass Tether Alternative 3 /5/09. 1. Engine Selection. Mission Parameters Required Thrust: 1.850 N Time of Flight : 351 days

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Gasses

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Solid-Propellant Rockets

Solid-Propellant Rockets. Nell Tebbets. History 400 B.C. steam-propelled wooden bird 100 B.C. aelopile first century A.D. fireworks 1232 first use as weapon of war 13th - 15th centuries much experimenting and improving less use as weapons 16th century step rocket

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Pop Can Hero Engine

Pop Can Hero Engine. By: Chelsey Lam, 4B.

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Science careers

Science careers. Jennifer Headrick. Earth science. meteorologist. Question time. Game time.

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Otto engine

Chris Treadwell. Otto engine. BACKGROUND. Nicolaus Otto first to develop functioning four stroke engine. German Engineer Developed 1876. THE ENGINE. Similar to modern engines Single cylinder Hit-and-miss Four stoke process Spark plug ignition Water jacket for cooling.

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