Overview
                                    This simple static thrust measurement 
									stand consists of a 
                                    balance with the rocket mounted on one side 
                                    with a kitchen scale on the other.  
				Test Stand
				The 
                                    kitchen scale measures 0 - 500grams. 
                                    Attached to the lever arm is a dampner that 
                                    prevents the spring in the scale from 
                                    oscillating as the rocket induces vibration 
                                    into the rig. 
                                    The scale dial is video taped at 60 
                                    frames per second which gives us a stable 
                                    time reference for the measurement samples. 
                                    These readings are then manually transferred to a spreadsheet 
                                    by replaying the video frame by frame. Ouch! 
                                    The balance can swing all the way around 
                                    on the pivot allowing us to permanently 
                                    mount the rocket on it, while giving us the 
                                    ability to easily fill it with water.  
                                    In this setup the nozzle is 85mm from the pivot point, 
                                    while the scale is at 1415mm from the pivot 
                                    point. 
                                    
										
											
												
												  | 
												The static thrust 
												measurement test stand. | 
											 
											
												
												  | 
												Detail view of the dampner 
												next to the kitchen scale.  | 
											 
											
												
												  | 
												Setting up the camera to 
												video tape the kitchen scale. | 
											 
										 
				 
				We chose a restricted nozzle to help 
                                    stretch out the data so it could be more 
                                    accurately measured and visualised.  
                                    The thrust measurement stand is balanced 
                                    so that it reads zero Newtons with the rocket 
                                    empty. This was done so that the data 
                                    obtained would reflect the thrust (force) 
                                    that contributes only to rocket 
                                    acceleration, as it already incorporates the 
                                    force needed to overcome the weight of the 
                                    water in the rocket. Hence the thrust measurement 
                                    does not represent the absolute thrust. 
                                    Ultimately we are only interested in how 
                                    much force is contributing to the 
                                    acceleration of the rocket upwards anyway.
                                     
                                    If we had balanced the stand while the 
                                    rocket is loaded with water, by the time the 
                                    thrust ended and all the water was out, the 
                                    scale would read the weight of the water 
                                    since it would now be unbalanced by that 
                                    amount. This would have introduced a bias to 
                                    the data. Since we do not know at what rate 
                                    the water empties from the rocket, we later 
                                    cannot remove this bias from the thrust 
                                    data.  
				
                                     References
									
				
                                    The original source of the article is from 
									Air Command Water Rockets website here: 
				
				
                                      
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