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The Helen Sharman Space Club Programme
The Helen Sharman Space Club Programme

Physics of Aircraft Instrumentation
Physics of Aircraft Instrumentation

Flight and Space
Flight and Space

here - Air and Surface Transport Nurses Association
here - Air and Surface Transport Nurses Association

... • The history of patient transport can be traced back to before the invention of the wheel when patients were carried or dragged to care. • Ambulance system were first established in the 1400’s using horse pulled stretchers and wagons specifically designed for patient transport. • During WW1 the U. ...
Analysis of the internal cooling system of a turbine blade Aerospace
Analysis of the internal cooling system of a turbine blade Aerospace

Example 1 – Zero Gravity flight
Example 1 – Zero Gravity flight

... At a safety briefing on the morning of my arrival, the pilot explains how the flight will proceed followed by a doctor who tells us how to survive the experience. Airplanes fly by forcing air over their wings in such a way that there is an excess of the upwards force, lift. Whi in the air, the plane ...
Vital for Flight
Vital for Flight

MAV Lecture - Fulton Student Organizations
MAV Lecture - Fulton Student Organizations

... Dynamic wing vehicles represent a leap in micro and nano-scale aerial vehicle design due to their size, agility and ability to carry small payloads such as surveillance equipment Vehicles that have hovering capabilities and can move at high velocity to a target efficiently are more desirable than th ...
Reliability Growth - Rocket Science and Technology
Reliability Growth - Rocket Science and Technology

... = Dn-1 p And, the expected number of defects corrected as a result of the nth flight test is = Dn-1 p d Then the expected number of latent lethal defects remaining after the nth flight is Dn = Dn-1 – Dn-1 p d = Dn-1 ( 1 – p d ) Thus, D1 = Do ( 1 – p d ), and D2 = D1 ( 1 – p d ) = Do ( 1 – p d )2 In ...
Newton’s Laws of Force
Newton’s Laws of Force

... a second object, the second one exerts a force on the first that is equal in size and opposite in direction –to every action force there is an opposite and equal reaction force ...
Worksheet-ImpulseAndMomentum
Worksheet-ImpulseAndMomentum

... N on it for 3 seconds? 8. A rocket engine exerts a force of 500 N on a space probe (in outer space!) for 5 seconds. The probe speeds up from rest to a speed of 21 m/s. What is its mass? 9. What force exerted for .12 seconds will make a .54 Kg baseball change its velocity 80 m/s? 10. What time must t ...
4.2.1.A-FourForcesofFlight
4.2.1.A-FourForcesofFlight

... • Factors that affect the amount of drag – the shape of the aircraft – the "stickiness“ of the air – the speed of the aircraft – The type of material used on the aircraft ...
race to space - cmasescience
race to space - cmasescience

... First US Hot Air Balloon Flight ...
Speeding Around the Sun
Speeding Around the Sun

... • If string let go  stopper would fly out like marble did with the tape • Yes stopper is accelerating  changing ...
Chapter 9 Momentum - Mrs. Krusa`s Wikispace
Chapter 9 Momentum - Mrs. Krusa`s Wikispace

... Is equal to the mass of an object times the velocity of an object Has the symbol “p” so p= m • v - measured in kg•m/s - It is a vector quantity ...
ITU Faculty of Aeronautics and Astronautics Department of
ITU Faculty of Aeronautics and Astronautics Department of

this page
this page

... module pilot William Anders) were supposed to test the lunar module in high Earth orbit in December. However, engineers would not have the lunar module ready in time for that launch window. Apollo's program manager, George Low, contemplated what to do with the mission. Should Apollo 8 repeat the tes ...
Four Forces of Flight
Four Forces of Flight

... • Factors that affect the amount of drag – the shape of the aircraft – the "stickiness“ of the air – the speed of the aircraft – The type of material used on the aircraft ...
Four Forces of Flight
Four Forces of Flight

... • Factors that affect the amount of drag – the shape of the aircraft – the "stickiness“ of the air – the speed of the aircraft – The type of material used on the aircraft ...
ECE 6390: Satellite Communications and Navigation Systems TEST
ECE 6390: Satellite Communications and Navigation Systems TEST

... 4. Deep Space Orbits: A “gravitational slingshot” is a method for propelling a spacecraft to outer planets without using extraordinary amounts of fuel, cost, and propulsion complexity. Under most circumstances, the orbit of a satellite around the solar system is an ellipse with the massive sun at o ...
Design and Development of a CubeSat De
Design and Development of a CubeSat De

... support structure. •Voltage differences can be converted to strain and then used to calculate drag coefficient produced by balloon ...
HSC Physics – Core Module 1 – Space
HSC Physics – Core Module 1 – Space

... remains the same. Additionally the gravitational field vector, g, reduces slightly with increasing altitude. The result is that a rockets rate of acceleration will increase and its velocity will increase too Consequently, the acceleration equation of a rocket will only be at an instant, provided tha ...
Velocity
Velocity

... Terminal Velocity • When a sky diver leaves the aircraft he speeds up because there are unbalanced forces acting. His weight is greater than the fictional drag force. • As his speed increases, the fictional drag due to the air increases. • Spreading himself like a eagle increases the surface area a ...
to see a sample homework problem set from Dynamics
to see a sample homework problem set from Dynamics

... 12.103 The Chandra X-ray observatory, launched in 1999, achieved an elliptical orbit of minimum altitude 6200 mi and maximum altitude 86,900 mi above the surface of the earth. Assuming that the observatory was transferred to this orbit from a circular orbit of altitude 6200 mi at point A, determine ...
Document
Document

... gravitational forces due to other planets can be neglected. The region inside of which the approximation is valid is called the sphere of influence (SOI) of the celestial body. If the spacecraft is not inside the SOI of a planet, it is considered to be in orbit around the sun. ...
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Flight dynamics (spacecraft)



Spacecraft flight dynamics is the science of space vehicle performance, stability, and control. It requires analysis of the six degrees of freedom of the vehicle's flight, which are similar to those of aircraft: translation in three dimensional axes; and its orientation about the vehicle's center of mass in these axes, known as pitch, roll and yaw, with respect to a defined frame of reference.Dynamics is the modeling of the changing position and orientation of a vehicle, in response to external forces acting on the body. For a spacecraft, these forces are of three types: propulsive force (usually provided by the vehicle's engine thrust); gravitational force exerted by the Earth or other celestial bodies; and aerodynamic lift and drag (when flying in the atmosphere of the Earth or other body, such as Mars or Venus). The vehicle's attitude must be taken into account because of its effect on the aerodynamic and propulsive forces. There are other reasons, unrelated to flight dynamics, for controlling the vehicle's attitude in non-powered flight (e.g., thermal control, solar power generation, communications, or astronomical observation).The principles of flight dynamics are normally used to control a spacecraft by means of an inertial navigation system in conjunction with an attitude control system. Together, they create a subsystem of the spacecraft bus often called ADCS.
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