X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2F2020-test-4.mdwn;fp=rockets%2Fresearch%2F2020-test-4.mdwn;h=e57f40cafca1a78a4c35ba974db5ef9dbf3a9681;hp=0000000000000000000000000000000000000000;hb=7373992fc904fe820cabb9664ede390405d6c61c;hpb=cb96cd832c0703ae747bad36079d96d7c4f147ab diff --git a/rockets/research/2020-test-4.mdwn b/rockets/research/2020-test-4.mdwn new file mode 100755 index 0000000..e57f40c --- /dev/null +++ b/rockets/research/2020-test-4.mdwn @@ -0,0 +1,35 @@ +# Test 2020-4 # + +3 grain 54mm Purple Pig motor with a Terry Lee dipped igniter in 3-inch test +mule flown on 17 October 2020 at the first-ever Tripoli Southern Colorado +launch at Hudson Ranch. In fact, this was the first-ever research flight +flown at this location! + +Used 3-grain 54mm Kosdon case, Loki-style nozzle with an 0.390" throat, +forward closure had a 1600psi pressure sensor and EasyMotor protototype +mounted with an A23 alkaline battery, and shooter wire as a "twist and tape" +power switch. + +The motor used three loose grains with 0.625" cores, thin o-rings as spacers, +and a greased phenolic liner. + +[Burnsim](2020-test-4-burnsim.pdf) called this a 31% J-355, 838 Ns with +about 2.36 sec burn time, and max pressure on a relatively flat burn of +559.3s psi. + +## Results ## + +Perfect flight, no damage, easy recovery. + +This was the first flight during which we successfully captured in-flight +chamber pressure data with an EasyMotor prototype board. A quick look at +the data shows about 540 psi maximum, which is pretty close to the Burnsim +prediction! Some software work remains to convert the data capture into +actual motor performance data. The EasyMotor data is logged in file +2020-10-17-serial-7085-flight-0007.eeprom + +The airframe's launch mass was about 4420 grams. The TeleMega on board +reported 9.54 G max and 6.29 G average acceleration to a max speed of +Mach 0.5 and a GPS apogee of 4669 feet. The TeleMega data is logged in file +2020-10-17-serial-6667-flight-0003.eeprom +