2018
DOI: 10.15282/jmes.12.4.2018.02.0348
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Electron spins coupling of coconut shell activated nanocarbons in solid propellant on improving to the thrust stability and specific impulses

Abstract: The role of activated coconut carbon in the combustion of solid propellant composed by ammonium perchlorate, aluminum, and hydroxyl terminated polybutadiene on improving to the thrust stability and specific impulses have been studied experimentally. Nanocarbons derived from coconut shells produces carbon compounds which dictates electron spin coupling sp2-sp3 when there is an increase in temperature until combustion occurs. Strong nanocarbon bonds require high temperatures and pressures to release bonds and bi… Show more

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“…The rocket was fired with the characteristics of composite AP propellant as oxidizer, HTPB as binder and Al as fuel. The rocket size is 20 mm cal with 50 mm fins, the rocket length is 500 mm and the throat nozzle diameter is 6 mm, the propellant mass is 100 grams producing a thrust of 40 N (Muda et al, 2018). The firing system is by directing the rocket launcher azimuth -90° to +90°, rocket elevation movement 0° to 50°, igniter for ignition or rocket activation by pressing the rocket button on the RC which is received by the receiver on the robot so that it works actively high (+ 5V), activates the igniter which can burn the rocket fuse.…”
Section: Figure 19 Rocket Firing Test Resultsmentioning
confidence: 99%
“…The rocket was fired with the characteristics of composite AP propellant as oxidizer, HTPB as binder and Al as fuel. The rocket size is 20 mm cal with 50 mm fins, the rocket length is 500 mm and the throat nozzle diameter is 6 mm, the propellant mass is 100 grams producing a thrust of 40 N (Muda et al, 2018). The firing system is by directing the rocket launcher azimuth -90° to +90°, rocket elevation movement 0° to 50°, igniter for ignition or rocket activation by pressing the rocket button on the RC which is received by the receiver on the robot so that it works actively high (+ 5V), activates the igniter which can burn the rocket fuse.…”
Section: Figure 19 Rocket Firing Test Resultsmentioning
confidence: 99%