Search for Free 150,000+ Essays

Find more results for this search now!
CLICK the BUTTON to the RIGHT!

Need a Brand New Custom Essay Now?  click here

Principles of Engineering a D12-5 Model Rcket Motor

Principles of engineering a D12-5 model rocket motor

The letter is the total impulse, the first number is the average thrust and the second number is the time delay. The motor in the figure is a class D total impulse engine with an average thrust of 12 Newtons(pounds) and a time delay of 5 seconds.

Total Impulse

The letter indicates the total impulse class of the engine, which is effectively the amount of fuel in the engine. The total impulse is the total momentum change that an engine can impart to a rocket. Total impulse is measured in Newton-seconds (pound-seconds). The standard impulse class for each letter is shown in the following table.

Class Total Impulse Newton-sec
1/4A 0.000 - 0.625
1/2A 0.626 - 1.25
A 1.260 - 2.50
B 2.510 - 5.00
C 5.010 - 10.0
D 10.01 - 20.0
E 20.01 - 40.0
F 40.01 - 80.0
G 80.01 - 160.0
H 160.01 - 320.0

Each class is double the impulse of the class below it, so as you increase the class of the engines, you double the amount of fuel each contains and double the amount of momentum you can give to a rocket

Average Thrust

The number following the letter indicates the average thrust of the engine in Newtons (pounds). Because the amount of fuel in an engine is fixed by the class letter, an engine with higher average thrust burns up its fuel more quickly than one with lower average thrust. As a result, the duration of a burn is roughly equal to the total impulse divided by the average thrust. The graph below shows the typical thrust profile for an engine with an average thrust of about 6 Newtons.

Typical engine thrust profile.

A typical engine starts with an initial high thrust for a fraction of a second, which is useful for getting things moving. It then settles down and burns the remainder of the propellant at a relatively constant rate.

Time Delay

The last number on an engine is the time delay, in seconds, to activation of the recovery system. The propellant in a model rocket typically burns up in about 1 second. At that point, the rocket is still moving upward at a high rate of speed. The time delay allows the rocket to continue up to its highest point before activating its recovery system. The time delay is achieved with a smoke charge that also...

Sign In Now to Read Entire Essay

Not a Member?   Create Your FREE Account »

Comments / Reviews

read full essay >>

Already a Member?   Login Now >

This essay and THOUSANDS of
other essays are FREE at eCheat.

Uploaded by:  

Date:  

Category:   Physics

Length:   2 pages (527 words)

Views:   3157

Report this Essay Save Essay
Professionally written essays on this topic:

Principles of Engineering a D12-5 Model Rcket Motor

View more professionally written essays on this topic »