Back in 1964, Estes released the B3 motor, which under the English unit nomenclature of the time meant that the motor had an average thrust of a whopping 3 pounds (13.3 newtons). The B3 was a Series II motor, which meant that a) it had high thrust and b) the manufacture required an additional step - drilling a deeper nozzle into the black powder propellant. The result was a motor with a short duration (~0.3 seconds), spike-like thrust curve with a peak thrust around 7 pounds (31 newtons) - the Estes catalog described the thrust as "like a sledge hammer blow." And it was true - the B3 could move single stage rockets so fast that poorly attached fins would rip right off, and easily had the power to loft heavy 3 stage payload carriers like the Farside-X. When I first started rocketry in '68, the motor classification system had just gone metric, so the B3 became the B14. Same characteristics, different label.
Comparison of B6 and B14 thrust curves in the 1968 Estes catalog (Click to enlarge). |
So why this foray into rocket motor history? It's because I have recently acquired some old Centuri B14 and Estes B8 motors, and I tested a couple of them - along with a current B6 - on my motor test stand last Saturday. I measured the thrust on the 50 newton maximum scale at 50 samples per second; the resulting curves are shown below. Note that the blue B14 curve is very similar to that shown in the catalog image above - a sharp spike up to 21 newtons, followed by an impulsive event at the end of the thrust (this was a booster motor, so no delay). However, there is a bit of a puzzle, as the peak thrust should have been over 30 newtons, whereas this Centuri motor produced only two-thirds that amount. I'm at a loss to explain this, except maybe to invoke motor deterioration over the 44 years since this motor was made. The red Estes B8 (manufactured in 1980) curve shows a similar sharp rise to 23 newtons peak, and then drops down to a thrust of just over 4 newtons, similar to that of the modern B6-4 (black curve). It is spent after 0.5 seconds, with the ejection charge occurring about 5.9 seconds after burnout.
Saturday's thrust measurements (Click to enlarge). |
2018 is gonna be a fun year!
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