Jump to content
Main menu
Main menu
move to sidebar
hide
Navigation
Main page
Recent changes
Random page
Help about MediaWiki
Special pages
Niidae Wiki
Search
Search
Appearance
Create account
Log in
Personal tools
Create account
Log in
Pages for logged out editors
learn more
Contributions
Talk
Editing
Model rocket
(section)
Page
Discussion
English
Read
Edit
View history
Tools
Tools
move to sidebar
hide
Actions
Read
Edit
View history
General
What links here
Related changes
Page information
Appearance
move to sidebar
hide
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
==Performance== The impulse (area under the thrust-time curve) of a model motor is used to determine its class. Motors are divided into classes from 1/4A to O and beyond. Black powder rocket motors are typically only manufactured up to Class F. Each class's upper limit is double the upper limit of the previous class. Model rockets only use motors that are class G and below.<ref>{{cite web |url=http://www.nar.org/modrocs.html |title=National Association of Rocketry |access-date=2013-09-25 |url-status=dead |archive-url=https://web.archive.org/web/20130928000247/http://www.nar.org/modrocs.html |archive-date=2013-09-28 }}</ref> Rockets using motors with a greater impulse are considered [[high power rockets]]. {| class="wikitable" style="text-align:center; float:right;" |- ! align=right| Class ! Total Impulse<br> (Metric Standard) |- style="text-align:right;" | 1/4A || 0.313-0.625 N·s |- style="text-align:right;" | 1/2A || 0.626-1.25 N·s |- style="text-align:right;" | A || 1.26-2.50 N·s |- style="text-align:right;" | B || 2.51-5.0 N·s |- style="text-align:right;" | C || 5.01-10 N·s |- style="text-align:right;" | D || 10.01-20 N·s |- style="text-align:right;" | E || 20.01-40 N·s |- style="text-align:right;" | F || 40.01-80 N·s |- style="text-align:right;" | G || 80.01-160 N·s |} Figures from tests of Estes rocket motors are used in the following examples of rocket motor performance.<ref name=Apogee>{{Cite web|url=http://www.apogeerockets.com/estes_items.asp|title = Estes Motors : Apogee Rockets, Model Rocketry Excitement Starts Here}}</ref> For miniature black powder rocket motors (13 mm diameter), the maximum [[thrust]] is between 5 and 12 N, the total impulse is between .5 and 2.2 Ns, and the burn time is between .25 and 1 second. For Estes ‘regular size’ rocket motors (18 mm diameter), there are three classes: A, B, and C. The A class 18 mm motors have a maximum thrust between 9.5 and 9.75 N, a total impulse between 2.1 and 2.3 Ns, and a burn time between .5 and .75 seconds. The B class 18 mm motors have a maximum thrust between 12.15 and 12.75 N, a total impulse between 4.2 and 4.35 Ns, and a burn time between .85 and 1 second. The C class 18mm motors have a maximum thrust from 14 – 14.15 N, a total impulse between 8.8 and 9 Ns, and a burn time between 1.85 and 2 seconds. There are also 3 classes included in Estes large (24 mm diameter) rocket motors: C, D, and E. The C class 24 mm motors have a maximum thrust between 21.6 and 21.75 N, a total impulse of between 8.8 and 9 Ns, and a burn time between .8 and .85 seconds. The D class 24 mm motors have a maximum thrust between 29.7 and 29.8 N, a total impulse between 16.7 and 16.85 Ns, and a burn time between 1.6 and 1.7 seconds. The E class 24 mm motors have a maximum thrust between 19.4 and 19.5 N, a total impulse between 28.45 and 28.6 Ns, and a burn time between 3 and 3.1 seconds. Estes has also released a line of 29mm black powder E and F motors. The 29mm E produces 33.4 Newton-seconds of total impulse over a 2.1 second burn, and the F produces 49.6 Newton-seconds over a 3.45 second burn. Several independent sources have published measurements showing that Estes model rocket engines often fail to meet their published thrust specifications.<ref name="TPT">Penn, Kim and William V. Slaton, Measuring Model Rocket Engine Thrust Curves, The Physics Teacher – December 2010 – Volume 48, Issue 9, pp. 591.</ref><ref name="Carter">[http://seit.unsw.adfa.edu.au/ojs/index.php/juer/article/download/108/69 An Investigation into the Combustion and Performance of Small Solid-Propellant Rocket Motors] M.G. Carter. University of New South Wales at the Australian Defence Force Academy. 2008.</ref><ref name = "Courtney">[https://arxiv.org/abs/0903.1555 Measuring thrust and predicting trajectory in model rocketry] M. Courtney and A. Courtney. Cornell University Library. 2009.</ref>
Summary:
Please note that all contributions to Niidae Wiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
Encyclopedia:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Search
Search
Editing
Model rocket
(section)
Add topic