# ABOUT MOTORS

### Basic Rocket Motor Knowledge

### About Rocket Motors

Rocket motors come in many sizes. They are measured in total impulse and are designated by letters of the alphabet. Each letter designates a range of total impulseThe total thrust produced by a rocket motor across its full burn time. Usually expressed in Newton-seconds.

*source*: rocketreviews.com and each motor size contains twice the total impulse of the previous letter. For example a

**B**motor has a potential total impulse twice that of the total impulse of an

**A**motor; a

**C**motor has twice the potential total impulse of a

**B**motor, etc. Rocket motors larger than

**G**are considered High Power; use of them requires certification

Levels one through three: reference to the three levels of high power rocketry certification. Unless you are in Canada, Eh?

*source*: rocketreviews.com by Tripoli

Tripoli Rocketry Association, Visit TRA

*source*: rocketreviews.com and/or NAR

National Association of Rocketry, Visit NAR

*source*: rocketreviews.com.

Low Power Rocketry | |||
---|---|---|---|

A | B | C | D |

1.25Ns ⟹ 2.5Ns | >2.5Ns ⟹ 5Ns | >5Ns ⟹ 10Ns | >10Ns ⟹ 20Ns |

Mid-Power Rocketry | ||
---|---|---|

E | F | G |

>20Ns ⟹ 40Ns | >40Ns ⟹ 80Ns | >80Ns ⟹ 160Ns |

###### High Power Rocketry

Certification Level 1 | |
---|---|

H | I |

>160Ns ⟹ 320Ns | >320Ns ⟹ 640Ns |

Certification Level 2 | ||
---|---|---|

J | K | L |

>640Ns ⇒ 1280Ns | >1280Ns ⇒ 2560Ns | >2560Ns ⇒ 5120Ns |

Certification Level 3 | ||
---|---|---|

M | N | O |

>5120Ns ⇒ 10240Ns | >10240Ns ⇒ 20480Ns | >20480Ns ⇒ 40960Ns |

Their potential power is indicated by a letter. However a motor of any given energy range might be configured to deliver only the middle of energy range rather than the full amount. That’s because you don’t always want the full amount. The motor manufacturer’s charts give you this information. The letter is followed by a number. The number tells you what the average thrust is. An example would be an

**I**170 or an

**I**240.

We are used to speaking in terms of horsepower and such, however, that’s only part of the equation, the amount of time applied given the amount of horsepower is needed to figure the total energy used. In rocketry, we use a different measurement and it is related to the total energy of the motor, i.e., power and time. Rocket motors are rated in Newton-seconds, however if you divide it by 4.45 and you will get pound-seconds. In other words so many pounds of force for one full second.

Hopefully, you are not lost and have acquired a good grasp of the concepts discussed to this point. To help you better comprehend all of this, here we will give you a little contrived comparison that makes it simple to understand.

Think of the term Newton•seconds

The typical unit of measurement for rocket thrust. One newtonsecond is one newton of thrust maintained for one second.

*source*: rocketreviews.com (or pound•seconds) as a way to express the amount of energy in four ounces of gasoline. One ounce of gasoline has 50.7 Newton-seconds of energy so four ounces of gasoline has 202.8 Newton•seconds (or 45.6 pound•seconds) of energy. With it, you can propel a car very fast for a brief time or slow for a long time. Either way you’ll burn up four ounces of gasoline and consume the same amount of energy (202.8 Newton•seconds or 45.6 pound•seconds). The choice is in how to use the energy, fast and brief, or slow and long.

**G**motor to launch a rocket and you’re choosing between a

**G**40 motor or a

**G**80 motor. Both are

**G**powered motors and both motors have 120 Newton•seconds of energy in this case. As stated previously, the number after the letter refers to the average thrust, so the two

**G**motor examples have a thrust of either 40 or 80 Newtons (not Newton•seconds). Divide 40 or 80 Newtons of thrust by 4.45 and you’ll get pounds of thrust. So the

**G**40 produces an average of 9 pounds of thrust and the

**G**80 produces an average of 18 pounds of thrust. If you had a one pound rocket you can now see the ratio of thrust to the weight of the rocket. The choice is again, fast and brief or slow and long. In general, the safe minimum lift-off weight ratio is 5:1. (ie. 5 lbs. of thrust for every 1 lb. of rocket.) Because the total energy contained in both these

**G**motors is 120 Newton•seconds (or 26.9 pound•seconds) it means the

**G**40 will burn for 3 seconds and the

**G**80 for 1.5 seconds. A lot of thrust for a brief period of time or half as much thrust for twice as long a period. For some detailed motor statistics go to www.thrustcurve.com.

##### Interpreting Rocket Motor Codes

Model rocket motors approved for sale in the United States are stamped with a three-part code that gives the rocketeer some basic information about the motor’s power and behavior. For example, an Estes**B**motor might be stamped:

- The letter
**B**specifies the impulse class. - The number
**6**tells us average thrust is 6 Newtons.

(6 Newtons equates to 1.3 pounds of thrust.) - The
**4**gives us the delay time between motor burnout and the firing of the ejection charge for recovery.

##### Delay Time

The rocket is traveling very fast at the moment the motor quits burning. The timed delay allows the rocket to coast to its maximum altitude and slow down before the parachute is ejected by the ejection charge. The ideal delay time for a rocket and a given motor can be calculated. Better yet, you can use OpenRocket, a free rocket modeling and simulation program, to predict both the altitude and coast time very accurately.##### Booster Motors

Model rocket motors marked with a time delay of 0 (e.g., “**C**6-0”) are booster engines for two stage rockets and are designed to ignite the next stage engine immediately once their own thrust is finished. In a multi-stage rocket, you would usually select a very long delay for your topmost engine.