git.gag.com Git - web/gag.com/blob - rockets/research/2017-test-12.mdwn

   1 # Test 2017-12 #
   2
   3 5 grain 75mm sorbitol motor with pyrodex pellet ignition in 4-inch Wildman
   4 rebuilt airframe at NCR North.
   5
   6 Trimmed CTI 5-grain case (25.75" overall), Loki #42 nozzle, CTI aft closure
   7 ring, forward bulkhead from Terry's pile machined to have 0.5" inside snap
   8 ring plus 0.25" inside liner, with two o-rings, one pushing against liner.
   9
  10 Liner 23.125" long with about 22.25" available for fuel load.
  11
  12 Simulation says this is a 57% L-1366 with 3804 Ns total impulse, 797 psi max,
  13 76% volume loading, and about 2.6 seconds burn time.
  14
  15 <!--Begin motor CTI mod Sorbitol HTML export from MotorSim-->
  16 <table class='motor' style='text-align: left; border: 1px solid black'><tr><th colspan='6' class='title'>CTI mod Sorbitol</th></tr><tr class='summary'><th>Rating:</th><td>57% L-1366</td><th>Max Pressure:</th><td>5.5 MPa</td></tr><tr class='summary'><th>Total Impulse:</th><td>3804 Ns</td><th>Specific Impulse:</th><td>131 s</td></tr><tr class='summary'><th>Max Thrust:</th><td>1706 N</td><th>Volume Loading:</th><td>76%</td></tr><tr class='summary'><th>Average Thrust:</th><td>1366 N</td><th>Fuel Mass:</th><td>2958 g</td></tr><tr><td colspan='4' class='thrust'><img src='http://chart.apis.google.com/chart?chxt=x,x,y,y,r,r&chs=400x200&cht=lxy&chco=3072F3&chds=0,2.78,0,1705.86&chxr=0,0,2.78|2,0,1705.86|4,0,383.49&chd=t:0,0,0,0,0,0,0.01,0.01,0.01,0.01,0.01,0.04,0.09,0.18,0.31,0.49,0.77,1.18,1.4,1.8,2.55,2.77,2.78|0,91.36,178.73,267.59,350.09,424.37,491.87,553.42,609.32,659.92,705.6,1075.86,1095.99,1121.65,1280.52,1398.83,1549.03,1685.96,1705.86,1637.7,490.86,0.61,0.48&chxl=1:|s|3:|N|5:|lbf&chxp=1,50|3,50|5,50' width='400' height='200' alt='null' /></td></tr></table>
  17 <!--End motor CTI mod Sorbitol-->
  18
  19 </p>
  20
  21 Neglected to re-weigh grains after trimming and before epoxying into the
  22 liner.
  23
  24 * Grain , g gross, g net, 4.5" long
  25 * Grain , g gross, g net, 4.5" long
  26 * Grain , g gross, g net, 4.5" long
  27 * Grain , g gross, g net, 4.4375" long
  28 * Grain , g gross, g net, 4" long
  29
  30 Total of g propellant, vs g simulated.
  31
  32 ## Results ##
  33
  34 Had to trim grains to fit.  Four just required squaring up the ends and
  35 trimming excess casting tube away.  Fifth one was cut in miter box with saw.
  36
  37 O-rings made forward closure a *very* snug fit.
  38
  39 Flight data logged as ? sn ?, flight ?.