Canadian Association of Rocketry
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1 Rocket Motor Certification August , 2009 Session Submitted to the CAR Executive August 31, 2009
2 2 Introduction A motor testing session was held at the facility in on August 27 and 28 th, It was a great session to attend in person! A total of forty (40) motors were fired to certify fourteen (14) new reloads. The list includes one F, one I, one L, seven M and four N motors. The propellants included four Blue Streaks, two Classics, three Imax, one Red Lightning and four Skidmarks. The total fired impulse was 246, N sec (50.4% R). The new additions include reloads for Pro29, Pro54, Pro75 and Pro98 from Cesaroni Technology Inc as well as one Pro98 reload cross certified for use in Aerotech RMS hardware and one Animal by Cesaroni (ABC) reload. Earlier this year, Dr. Louwers proposed the introduction of a simple grain spacer for use in CTI hardware. The spacers are the length of a single grain, and are loaded into the case forward of the reload. This means that all of the pressure remains within the reload, but the ejection charge (if present) can freely pass through. In the course of normal testing, 75mm and 98mm spacers were included without incident. Two stacked 1G spacers (38mm) were hydrostatically tested in a 3G case to failure, and the failure point was the nozzle (longitudinal failure mode) as described by NFPA 1125, section After disassembling the destroyed 3G case, the spacers slid out undamaged, even after exposure to 2,380 PSI (over 3X the working pressure of the reload). The Pro29 tapered closures have been used in Pro29 testing and have performed normally. As a result of this testing, 38mm, 75mm and 98mm spacers (alone or stacked) and the Pro29 tapered closure form part of the certified motor systems from CTI. These spacers (38mm, 75mm and 98mm) and optional closures (29mm) will continue to be included in upcoming tests to observe the effect of accelerated usage. While these motors were certified in Canada, a reciprocal agreement between the Canadian Association of Rocketry, the Tripoli Rocketry Association and the National Association of Rocketry means they may be flown in many jurisdictions. I am very pleased to announce the certification of these fourteen (14) new reloads from Cesaroni Technology, Inc. Individual certification letters follow for each motor. These letters and the accompanying thrust curves will be available on the official CAR website soon. Chair of
3 3 Contents Introduction... 2 Certified Motors... 4 CTI 55-F29-IM-12A (CTI Pro29-1G)... 4 CTI 381-I224-CL-15A (CTI Pro29-6GXL)... 5 CTI 3147-L935-IM-P (CTI Pro54-6GXL)... 6 CTI 8,088-M1790-SK-P (CTI Pro98-4G / AT-98/10240)... 7 CTI 11,077-N2600-SK-P (CTI Pro98-6G)... 8 CTI-14,263-N3400-SK-P (CTI Pro98-6GXL)... 9 CTI 7,579-M1520-BS-P (CTI Pro98-3G) CTI 9,870-M1800-BS-P (CTI Pro98-4G) CTI 13,767-N2850-BS-P (CTI Pro98-6G) CTI 17,613-N2900-CL-P (CTI Pro98-6GXL) CTI 5506-M1230-IM-P (CTI Pro75-4G) CTI 7,455-M2150-RL-P (CTI Pro75-6G) CTI 7,388-M2045-BS-P (CTI Pro75-6G) ABC 6,774-M2050-SK-P (AMW )... 17
4 4 Certified Motors CTI 55 F29 IM 12A (CTI Pro29 1G) The CTI 55-F29-IM-12A rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 55 F29 IM 12A Test Date August 27, 2009 Manufacturer Designation CTI 55 F29 12A Manufacturer Cesaroni Technology Inc. Propellant Imax Hardware Pro29 1G Single Use/Reload/Hybrid Reloadable Motor Dimensions 29mm x 98mm Loaded Weight g Total Impulse 54.8 Ns (12.3 lb s) Burnout Weight 68.2 g Maximum Thrust 36.0 N (8.1 lb) Propellant Weight 30.9 g Average Thrust 28.9 N (6.5 lb) Delays Tested 12 3 seconds, adjustable Specific Impulse (Isp) s Samples per second 1000 Burn time 1.90 s 37.0% F Chairman, gra
5 5 CTI 381 I224 CL 15A (CTI Pro29 6GXL) The CTI 381-I224-CL-15A rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 381 I224 CL 15A Test Date August 27, 2009 Manufacturer Designation CTI 381 I224 15A Manufacturer Cesaroni Technology Inc. Propellant Classic Hardware Pro29 6GXL Single Use/Reload/Hybrid Reloadable Motor Dimensions 29mm x 365mm Loaded Weight g Total Impulse Ns (85.8 lb s) Burnout Weight g Maximum Thrust N (102.1 lb) Propellant Weight g Average Thrust N (50.3 lb) Delays Tested 15 6 seconds, adjustable Specific Impulse (Isp) s Samples per second 1000 Burn time 1.70 S 19.2% I Chairman, gra
6 6 CTI 3147 L935 IM P (CTI Pro54 6GXL) The CTI 3147-L935-IM-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 3147 L935 IM P Test Date August 27, 2009 Manufacturer Designation CTI 3147 L935 P Manufacturer Cesaroni Technology Inc. Propellant Imax Hardware Pro54 6GXL Single Use/Reload/Hybrid Reloadable Motor Dimensions 54mm x 649mm Loaded Weight g Total Impulse Ns (707.4 lb s) Burnout Weight g Maximum Thrust N (356.5 lb) Propellant Weight 1567 g Average Thrust N (209.9 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time s 22.9% L Chairman, gra
7 7 CTI 8,088 M1790 SK P (CTI Pro98 4G / AT 98/10240) The CTI 8,088-M1790-SK-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 8,088 M1790 SK P Test Date August 27, 2009 Manufacturer Designation CTI 8,088 M1790 P Manufacturer Cesaroni Technology Inc. Propellant Skidmark Hardware Pro98 4G / AT 98/10240 Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 702mm (98 x 732) Loaded Weight 8,273 g / 8,298 g Total Impulse 8,088.9 Ns (1,818.5 lb s) Burnout Weight 3,456 g / 3,477 g Maximum Thrust 2,092.7 N (470.5 lb) Propellant Weight 4,706 g Average Thrust 1,786.3 N (401.6 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 4.53 s 58.0% M Cross certified for use in CTI and Aerotech hardware Chairman, gra
8 8 CTI 11,077 N2600 SK P (CTI Pro98 6G) The CTI 11,077-N2600-SK-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 11,077 N2600 SK P Test Date August 27, 2009 Manufacturer Designation CTI 11,077 N2600 P Manufacturer Cesaroni Technology Inc. Propellant Skidmark Hardware CTI Pro98 6G Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 1010mm Loaded Weight 11,482 g Total Impulse 11,077.3 Ns (2,490.3 lb s) Burnout Weight 4,712 g Maximum Thrust 3,047.7 N (685.1 lb) Propellant Weight 6,618 g Average Thrust 2,585.5 N (581.2 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 4.28 s 8.2% N Chairman, gra
9 9 CTI 14,263 N3400 SK P (CTI Pro98 6GXL) The CTI-14,263-N3400-SK-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 14,263 N3400 SK P Test Date August 27, 2009 Manufacturer Designation CTI 14,263 N3400 P Manufacturer Cesaroni Technology Inc. Propellant Skidmark Hardware CTI Pro98 6GXL Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 1239mm Loaded Weight 13,972 g Total Impulse 14,263.3 Ns (3,206.5 lb s) Burnout Weight 5,501 g Maximum Thrust 3,741.6 N (841.2 lb) Propellant Weight 8,282 g Average Thrust 3,403.1 N (765.0 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 4.19 s 39.3% N Chairman, gra
10 10 CTI 7,579 M1520 BS P (CTI Pro98 3G) The CTI 7,579-M1520-BS-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 7,579 M1520 BS P Test Date August 27, 2009 Manufacturer Designation CTI 7,579 M1520 P Manufacturer Cesaroni Technology Inc. Propellant Blue Streak Hardware CTI Pro98 3G Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 548mm Loaded Weight 6,718 g Total Impulse 7,579.0 Ns (1,703.8 lb s) Burnout Weight 2,981 g Maximum Thrust 1,824.9 N (410.3 lb) Propellant Weight 3,602 g Average Thrust N (343.1 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 4.97 s 48.0% M Chairman, gra
11 11 CTI 9,870 M1800 BS P (CTI Pro98 4G) The CTI 9,870-M1800-BS-P rocket motor was tested August 28 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 9,870 M1800 BS P Test Date August 28, 2009 Manufacturer Designation CTI 9,870 M1800 BS P Manufacturer Cesaroni Technology Inc. Propellant Blue Streak Hardware CTI Pro98 4G Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 702mm Loaded Weight 8,342 g Total Impulse 9,869.7 Ns (2,218.8 lb s) Burnout Weight 3,383 g Maximum Thrust 2,240.6 N (503.7 lb) Propellant Weight 4,802 g Average Thrust 1,797.1 N (404.0 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 5.49 s 92.8% M Chairman, gra
12 12 CTI 13,767 N2850 BS P (CTI Pro98 6G) The CTI 13,767-N2850-BS-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 13,767 N2850 BS P Test Date August 27, 2009 Manufacturer Designation CTI 13,767 N2850 BS P Manufacturer Cesaroni Technology Inc. Propellant Blue Streak Hardware CTI Pro98 6G Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 1010mm Loaded Weight 11,688 g Total Impulse 13,766.9 Ns (3,094.9 lb s) Burnout Weight 4,723 g Maximum Thrust 3,377.2 N (759.2 lb) Propellant Weight 6,759 g Average Thrust 2,835.9 N (637.5 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 4.85 s 34.4% N Chairman, gra
13 13 CTI 17,613 N2900 CL P (CTI Pro98 6GXL) The CTI 17,613-N2868-CL-P rocket motor was tested August 27 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 17,613 N2900 CL P Test Date August 27, 2009 Manufacturer Designation CTI 17,613 N2900 CL P Manufacturer Cesaroni Technology Inc. Propellant Classic Hardware CTI Pro98 6GXL Single Use/Reload/Hybrid Reloadable Motor Dimensions 98mm x 1239mm Loaded Weight 14,166 g Total Impulse 17,613.7 Ns (3,959.7 lb s) Burnout Weight 5,378 g Maximum Thrust 4,164.5 N (936.2 lb) Propellant Weight 8,449 g Average Thrust 2,867.5 N (644.6 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 6.14 s 72.0% N Chairman, gra
14 14 CTI 5506 M1230 IM P (CTI Pro75 4G) The CTI 5506-M1230-IM-P rocket motor was tested August 28 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 5506 M1230 IM P Test Date August 28, 2009 Manufacturer Designation CTI 5506 M1230 IM P Manufacturer Cesaroni Technology Inc. Propellant Imax Hardware CTI Pro75 4G Single Use/Reload/Hybrid Reloadable Motor Dimensions 75mm x 621mm Loaded Weight 4,844 g Total Impulse 5,506.5 Ns (1,237.9 lb s) Burnout Weight 1,852 g Maximum Thrust 1,586.6 N (356.7 lb) Propellant Weight 2900 g Average Thrust 1,229.6 N (276.4 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 4.48 s 7.5% M Chairman, gra
15 15 CTI 7,455 M2150 RL P (CTI Pro75 6G) The CTI 7,455-M2150-RL-P rocket motor was tested August 28 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 7,455 M2150 RL P Test Date August 28, 2009 Manufacturer Designation CTI 7,455 M2150 RL P Manufacturer Cesaroni Technology Inc. Propellant Red Lightning Hardware CTI Pro75 6G Single Use/Reload/Hybrid Reloadable Motor Dimensions 75mm x 893mm Loaded Weight 6,324 g Total Impulse 7,455.4 Ns (1,676.0 lb s) Burnout Weight 2,355 g Maximum Thrust 2,614.1 N (587.7 lb) Propellant Weight 3,835 g Average Thrust 2,147.0 N (482.7 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 3.47 s 45.6% M Chairman, gra
16 16 CTI 7,388 M2045 BS P (CTI Pro75 6G) The CTI 7,388-M2045-BS-P rocket motor was tested August 28 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation CTI 7,388 M2045 BS P Test Date August 28, 2009 Manufacturer Designation CTI 7,388 M2045 BS P Manufacturer Cesaroni Technology Inc. Propellant Blue Streak Hardware CTI Pro75 6G Single Use/Reload/Hybrid Reloadable Motor Dimensions 75mm x 893mm Loaded Weight 6,071 g Total Impulse 7,388.0 Ns (1,660.9 lb s) Burnout Weight 2,332 g Maximum Thrust 2,951.8 N (663.6 lb) Propellant Weight 3,547 g Average Thrust 2,046.6 N (460.1 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 3.61 s 44.3% M Chairman, gra
17 17 ABC 6,774 M2050 SK P (AMW ) The ABC 6,774-M2050-SK-P rocket motor was tested August 28 th, 2009 and is in compliance with the certification requirements and standards of the (CAR). The motor is hereby CAR Designation ABC 6,774 M2050 SK P Test Date August 28, 2009 Manufacturer Designation ABC 6,774 M2050 SK P Manufacturer Cesaroni Technology Inc. Propellant Skidmark Hardware AMW Single Use/Reload/Hybrid Reloadable Motor Dimensions 76mm x 1039mm Loaded Weight 7,129 g Total Impulse 6,774.6 Ns (1,523.0 lb s) Burnout Weight 2,957 g Maximum Thrust 2,554.4 N (574.2 lb) Propellant Weight 3,870 g Average Thrust 2,049.8 N (460.8 lb) Delays Tested plugged Specific Impulse (Isp) s Samples per second 1000 Burn time 3.31 s 32.3% M Chairman, gra
18 18
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