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Beginner's Guide to Rockets
Mach Number

Answers

  1. Use the definition of Mach number obtained from the Mach number slide and the information in the activity to determine the speed of a rocket flying at Mach 3 at sea level. ~2280 mph or 3669 km/hr.

  2. Convert the sea level speed of sound, 760 mph, from units of mph to km/hr. ~1223 km/hr.

  3. Let's perform a little study to determine how the velocity of a rocket changes during its flight into orbit. We've installed a small device on the side of the rocket to measure the free stream Mach number. The data is presented below in terms of time after launch and measured Mach number. Convert this data to velocity (km/hr) assuming the speed of sound remains the same as the velocity you computed in problem #2:

    Time s
    Mach
    Speed, km/hr
    60
    1.0
    1223
    120
    2.8
    3424
    180
    4.5
    5504
    240
    6.5
    7950
    300
    9.0
    11007
     

  4. We know that the temperature and speed of sound change with altitude, so let's correct our data for that effect. We have some additional radar data that gives the altitude of our rocket during its ascent. Use the AtmosModeler simulator to determine the actual speed of sound at each altitude and calculate a more accurate value of the rocket's velocity:

    Time s
    Mach
    Altitude m
    Speed of Sound, km/hr
    Speed of Rocket, km/hr
    60
    1.0
    1000
    1211
    1211
    120
    2.8
    2500
    1190
    3332
    180
    4.5
    5000
    1154
    5193
    240
    6.5
    15000
    1062
    6903
    300
    9.0
    30000
    1098
    9882

     

  5. The RocketThrust computer simulation was used to model the exhaust from the Space Shuttle Main Engine (SSME) nozzle. The exit Mach number is 4.54, and the exit velocity is 12,250 feet/sec.


    A. What is the speed of sound in the exhaust (feet/sec)?

    Exhaust Speed of Sound = 2698 ft/sec


    B. How does that compare with the speed of sound in air at sea level, expressed in feet/sec?

    Air Speed of Sound = 1115 ft/sec


    C. Why do you think they are different?

    The exhaust from the rocket nozzle is at a much higher temperature.

    The exhaust is not air (nitrogen, oxygen, etc), it is mostly steam (H2O) which has very different chemical properties than air.



Related Sites:
Teaching Standards
Activity
Worksheet
Rocket Index
Rocket Home
Exploration Systems Mission Directorate Home

 

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Editor: Tom Benson
NASA Official: Tom Benson
Last Updated: May 13 2021

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