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Rocketry Unit

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The stabilizing and guiding unit of a model rocket. ... The '6' in our example motor tells us that the energy is delivered at a moderate ... – PowerPoint PPT presentation

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Title: Rocketry Unit


1
Rocketry Unit
  • Physics
  • McFall
  • 7th Period

2
Newton's First Law
  • Objects at rest will stay at rest, and objects in
    motion will stay in motion in a straight line
    unless acted upon by an unbalanced force.
  • In rocket flight, forces become balanced and
    unbalanced all the time. A rocket on the launch
    pad is balanced. The surface of the pad pushes
    the rocket up while gravity tries to pull it
    down. As the engines are ignited, the thrust from
    the rocket unbalances the forces, and the rocket
    travels upward. Later, when the rocket runs out
    of fuel, it slows down, stops at the highest
    point of flight, then falls back to the Earth.

3
Newton's Second Law
  • F ma - Force is equal to mass times
    acceleration.
  • Force in the equation can be thought of as the
    thrust of the rocket engine. Mass in the equation
    is the amount of rocket fuel being burned and
    converted into gas that expands and then escapes
    from the rocket. Acceleration is the rate at
    which the gas escapes. Inside the rocket, the gas
    does not really move, but as it leaves the engine
    it picks up speed.
  • Newton's second law of motion can be restated in
    the following way the greater the mass of rocket
    fuel burned and the faster the gas produced can
    escape the engine, the greater the thrust of the
    engine.

4
Newton's Third Law
  • For every action there is always an opposite and
    equal reaction.
  • With rockets, the action is the expelling of gas
    out of the engine. The reaction is the movement
    of the rocket in the opposite direction. To
    enable a rocket to lift off from the launch pad,
    the action, or thrust, from the engine must be
    greater than the weight of the rocket.

5
Putting Newton's Laws of Motion Together
  • An unbalanced force must be exerted for a rocket
    to lift off from the launch pad (first law). The
    amount of thrust (force) produced by a rocket
    engine will be determined by the mass of the
    rocket fuel that is burned and how fast the gas
    escapes the rocket (second law). The reaction, or
    motion, of the rocket is equal to and in an
    opposite direction from the action, or thrust,
    from the engine (third law).

6
  • Parts of a Model Rocket

7
Nose Cone
  • The foremost surface of a model rocket, generally
    tapered in shape, usually made of balsa or
    plastic. It reduces drag by directing airflow
    smoothly around rocket.

8
Body
  • A specially wound and treated cardboard or
    plastic cylinder used to make the fuselage or
    airframe of a model rocket to which all other
    parts are attached.

9
Recovery System
  • The device in a model rocket whose purpose is to
    return the rocket to the ground safely by
    creating excess drag or by creating lift. All
    model rockets must employ a recovery system, such
    as a parachute.

10
Launch Lug
  • Round, hollow tube (attached to the model rocket)
    which slips over the launch rod to guide the
    model during the first few feet of flight until
    sufficient airspeed is reached allowing the fins
    to operate.

11
Recovery Wadding
  • Flame resistant tissues that are packed between
    the model rocket engine and the streamer or
    parachute to protect the recovery device from the
    hot gases of the ejection charge.

12
Fins
  • The stabilizing and guiding unit of a model
    rocket. The aerodynamic surfaces projecting from
    the rocket body for the purpose of giving the
    rocket directional stability. Usually made of
    balsa wood or plastic, and located at the rear of
    the rocket.

13
Engine Mount
  • Safely secures the engine in a model rocket.
    Sometimes includes an engine hook.

14
Total Impulse
  • Total impulse is a measure of the overall total
    energy contained in a motor, and is measured in
    Newton-seconds. The letter "C" in our example
    engine above tells us that there is anywhere from
    5.01 to 10.0 N-sec of total impulse available in
    this engine.
  • Since each letter represents twice the power
    range of the previous letter, total available
    power increases rapidly the further you progress
    through the alphabet.

15
Average Thrust
  • Average thrust is a measure of how slowly or
    quickly the motor delivers its total energy, and
    is measured in Newtons. The "6" in our example
    motor tells us that the energy is delivered at a
    moderate rate (over about 1.7 seconds). A C4
    would deliver weaker thrust over a longer time
    (about 2.5 seconds), while a C10 would deliver a
    strong thrust for a shorter time (about a
    second).
  • As a rule of thumb, the thrust duration of a
    motor can be approximated by dividing its total
    impulse by its average thrust.
  • Keep in mind that you cannot assume that the
    actual total impulse of a motor lies at the top
    end of its letter's power range - an engine
    marked "C" might be engineered to deliver only
    5.5 Newton-seconds, not 10.

16
Motor Parts
17
  • Paper Casing
  • A paper cover that protects the charges of a
    model rocket engine and confines the internal
    pressure during combustion allowing the exhaust
    gas to escape through the nozzle.
  •  
  • Clay Nozzle
  • A device on the bottom end of an engine that
    channels the exhaust gas through the nozzle
    throat to greatly increase the exhaust gas speed
    which in turn develops thrust.
  •   Propellant
  • A chemical paste of a combustible nature, that
    has been commercially developed and loaded in the
    casing of a model rocket engine that when ignited
    will provide the thrust necessary to launch a
    model rocket.

18
  • Coast or Delay Phase
  • A no thrust, slow burning charge that emits smoke
    to aid in tracking and allows the rocket to coast
    to a higher altitude before activation of the
    ejection charge for recovery system deployment.
  •  
  • Ejection Charge
  • Ignited by the delay element and produces
    expanding gases which activate or eject a
    recovery device.
  •   Clay Retaining Cap
  • A clay cap that prevents the combustion gasses
    from escaping. It is destroyed by the ejection
    charge. It is located opposite the nozzle.
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