Simulator Data

Statistics	Declared	Calculated	Official
Motor:	AeroTech H112
Contributor:	John Coker
Submitted:	May 30, 2006
Last Updated:	May 30, 2006
Data Format:	CompuRoc
Data Source:	Certification Org
License:	Public Domain
Diameter (mm):	—		38.0
Length (cm):	—		19.1
Prop. Weight (g):	—		191.2
Total Weight (g):	—		379.5
Avg. Thrust (N):	—	86.9	112.0
Max. Thrust (N):	—	105.6	121.7
Tot. Impulse (Ns):	—	263.0	261.1
Burn Time (s):	—	3.0	2.9
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Data Graph

Alternates: in Pounds large size

Data File

THRUST
; AeroTech H112J
; converted from TMT test stand data 1999 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
; total weight: 379g, propellant weight: 188g
0.00	0.00
0.02	56.04
0.07	102.17
0.12	104.86
0.17	101.44
0.22	101.10
0.27	101.10
0.32	102.02
0.37	101.94
0.42	102.87
0.47	102.65
0.52	103.61
0.57	103.98
0.62	105.14
0.66	104.05
0.71	104.21
0.76	103.28
0.81	102.65
0.86	104.12
0.91	103.79
0.96	103.76
1.01	104.95
1.06	105.46
1.11	104.86
1.16	104.39
1.21	105.65
1.26	104.07
1.31	103.23
1.36	101.80
1.41	103.33
1.45	101.68
1.50	102.68
1.55	101.89
1.60	99.95
1.65	99.75
1.70	99.53
1.75	98.19
1.80	97.86
1.85	95.03
1.90	95.17
1.95	91.62
2.00	90.03
2.05	87.95
2.10	84.95
2.14	83.13
2.19	80.53
2.24	78.49
2.29	78.04
2.34	75.25
2.39	72.89
2.44	70.98
2.49	68.44
2.54	66.68
2.59	65.66
2.64	62.83
2.69	58.66
2.74	51.57
2.79	40.23
2.84	29.01
2.89	20.62
2.94	13.39
2.98	8.25
3.03	5.24
3.08	3.63
3.13	3.15
3.18	1.81
3.23	1.16
-1.00

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