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Title: Continuous%20Mass%20Flow%20Rockets%208.01%20W08D1


1
Continuous Mass Flow Rockets8.01W08D1
2
Juno Lift-Off
http//anon.nasa-global.edgesuite.net/HD_downloads
/juno_launch_1080i.wmv
3
Todays Reading Assignment W08D1
  • Young and Freedman 8.6
  • Class Notes Continuous Mass Flow

4
Worked Example Stream Bouncing off Wall
  • A stream of particles of mass m and separation d
    hits a perpendicular surface with speed v. The
    stream rebounds along the original line of motion
    with the same speed. The mass per unit length of
    the incident stream is l m/d. What is the
    magnitude of the force on the surface?

5
Category 1 Adding Mass But Not Momentum
  • There is a transfer of material into the object
    but no transfer of momentum in the direction of
    motion of the object. Consider for example rain
    falling vertically downward into a moving cart. A
    small amount of rain has no component of
    momentum in the direction of motion of the cart.

6
Concept Question
  • Suppose rain falls vertically into an open cart
    rolling along a straight horizontal track with
    negligible friction. As a result of the
    accumulating water, the speed of the cart
  • increases.
  • does not change.
  • decreases.
  • not sure.
  • not enough information is given to decide.

7
Fire Plane Scooping up Water
8
Category 2 Losing Mass But Not Momentum
  • The material continually leaves the object but
    it does not transport any momentum away from the
    object in the direction of motion of the object.
    For example, consider an ice skater gliding on
    ice holding a bag of sand that is leaking
    straight down with respect to the moving skater.

9
Category 3 Impulse
  • The material continually hits the object
    providing an impulse resulting in a transfer of
    momentum to the object in the direction of
    motion. For example, suppose a fire hose is used
    to put out a fire on a boat. The incoming water
    continually hits the boat impulsing it forward.

10
Category 4 Recoil
  • The material continually is ejected from the
    object, resulting in a recoil of the object. For
    example when fuel is ejected from the back of a
    rocket, the rocket recoils forward.

11
Rocket Equation
12
(No Transcript)
13
Worked Example Rocket Motion
  • A rocket at time t is moving with speed vr,0 in
    the positive x-direction in empty space. The
    rocket burns the fuel at a rate dmf,out /dt b gt
    0. The fuel is ejected backward with speed u
    relative to the rocket.
  • a) What is the relationship between the time
    rate of change of exhaust mass dmf /dt, and the
    time rate of change of rocket mass dmr /dt?
  • b) Find an equation for the rate of change of
    the speed of the rocket in terms mr (t) ,u, and
    dmr /dt and solve for v.
  • c) Find the differential equation describing the
    motion of the rocket if it is in a constant
    gravitational field of magnitude g

14
Strategy Rocket Motion
  • Goal Determine velocity of rocket as function of
    time as mass is continuously ejected at rate dmf
    /dt with speed u relative to rocket.
  • System consider all elements that undergo
    momentum change rocket and fuel
  • Using Momentum flow diagram, apply
  • to find differential equation that describes
    motion.

15
Rocket Motion
  • A rocket at time t 0 is moving with speed vr,0
    in the positive x-direction in empty space. The
    rocket burns the fuel at a rate dmf /dt b gt0.
    The fuel is ejected backward with speed u
    relative to the rocket. The goal is to find an
    equation for the rate of change of the speed of
    the rocket in terms mr (t) ,u, and dmr /dt and
    solve for v.

16
State at time t
  • Rocket with total mass mr(t) moves with speed
    vr(t) in positive x-direction according to
    observer
  • 2. Total mass consists of mass of rocket mr,0
    and fuel mf (t)
  • 3. Fuel element with mass ?mf, moves with speed
    of rocket vr (t) at time t, is ejected during
    interval t, t?t
  • 4. x-component of momentum at time t

17
State at t ?t
  • Rocket is propelled forward by ejected fuel with
    new rocket speed
  • Fuel is ejected backward with speed u relative
    to rocket. Relative to observers frame, ejected
    fuel element has speed
  • x-component of systems momentum at time t?t

18
Rocket Equation
  • Are there any external forces at time t? Two
    cases
  • Taking off
  • (2) Negligible gravitational field
  • Apply Momentum Principle

19
Rocket Equation Conservation of Mass and Thrust
  • Conservation of mass Rate of decrease of mass
    of rocket equals rate of ejection of mass
  • Rocket equation
  • Fuel Ejection Thrust force

20
Solution Rocket Motion in Gravitational Field
  • Rocket Equation
  • Fuel ejection term can be interpreted as thrust
    force
  • Relative fuel ejection velocity
  • External force
  • Rocket equation
  • Integrate with respect to time
  • Solution

21
Concept Question Rocket Fuel Burn Time
  • When a rocket accelerates in a constant
    gravitational field, will it reach a greater
    final velocity if the fuel burn time is
  • as fast as possible?
  • as slow as possible?
  • The final speed is independent of the fuel burn
    time?
  • Im not sure.

22
Answer Rocket Equation in Gravitational Field
  • Fuel ejection term can be interpreted as thrust
    force
  • Solution shorter the burn time, the greater the
    velocity

23
Concept Question Rocket with Constant Thrust
  • If a rocket in gravity-free outer space has a
    constant thrust at all times while burning fuel,
    is its acceleration
  • constant?
  • increasing?
  • decreasing?

24
Table Problem Rocket Sled
  • A rocket sled ejects gas backwards at a speed u
    relative to the rocket sled. The mass of the fuel
    in the rocket sled is equal to one half the
    initial total mass mr,0 (including fuel) of the
    sled. The rocket sled starts from rest on a
    frictionless track. You may ignore air
    resistance.
  • Derive a relation between the differential of
    the speed of the rocket sled, dvr , and the
    differential of the total mass of the rocket, dmr
  • Integrate the above relation to find the speed
    of the rocket sled as a function of mass, vr(m),
    as the rocket sled speeds up.
  • What is the final speed of the rocket sled after
    all the fuel has been burned? Express your
    answers in terms of the quantities u, and mr,0
    as needed.
  • After reaching its final speed, the sled enters a
    rough portion of the track that begins at x 0
    with a coefficient of kinetic friction that
    varies with distance
  • µk(x)bx where b is a positive constant.
    How far D did the sled slide before it came to
    rest in that portion of the track? Express your
    answers in terms of the quantities u, b, g, and
    mr,0 as needed.

25
Next Class W08D2Test Two ReviewCircular Motion,
Energy, Momentum, and Collisions
26
Next Reading Assignment W09D1
  • Young and Freedman 1.10 (Vector Products)
    9.1-9.6, 10.5
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