National Fire Protection Association 1 Batterymarch Park, Quincy, MA 02169-7471 Phone: 617-770-3000 Fax: 617-770-0700 www.nfpa.org M E M O R A N D U M TO: FROM: Technical Committee on Pyrotechnics Yvonne Smith, Project Administrator DATE: January 28, 2015 SUBJECT: NFPA 1122 First Draft Technical Committee FINAL Ballot Results (A2017) According to the final ballot results, all ballot items received the necessary affirmative votes to pass ballot. 30 Members Eligible to Vote 5 Members Not Returned (Davidson, Hill, Pier, Rogers, Wright) 24 Members Voted Affirmative on All Revisions 0 Members Voted Negative on one or more Revisions 1 Members Abstained on one or more Revisions (Miller) The attached report shows the number of affirmative, negative, and abstaining votes as well as the explanation of the vote for each revision. To pass ballot, each revision requires: (1) a simple majority of those eligible to vote and (2) an affirmative vote of 2 /3 of ballots returned. See Sections 3.3.4.3.(c) and First Draft reference 4.3.10.1 of the Regulations Governing the Development of NFPA Standards.
1 of 15 1/28/2016 11:48 AM First Revision No. 11-NFPA 1122-2015 [ Chapter 2 ] Chapter 2 Referenced Publications 2.1 General. The documents or portions thereof listed in this chapter are referenced within this code and shall be considered part of the requirements of this document. 2.2 NFPA Publications. National Fire Protection Association, 1 Batterymarch Park, Quincy, MA 02169-7471. NFPA 1123, Code for Fireworks Display, 2010 2018 edition. NFPA 1124, Code for the Manufacture, Transportation, Storage, and Retail Sales of Fireworks and Pyrotechnic Articles, 2013 2017 edition. NFPA 1125, Code for the Manufacture of Model Rocket and High Power Rocket Motors, 2012 2017 edition. NFPA 1126, Standard for the Use of Pyrotechnics Before a Proximate Audience, 2011 2016 edition. NFPA 1127, Code for High Power Rocketry, 2013 2018 edition. 2.3 Other Publications. 2.3.1 U.S. Government Publications. U.S. Government Printing Publishing Office, 732 North Capitol Street, NW, Washington, DC 20402 20401-0001. Title 14, Code of Federal Regulations, Chapter 1, Subchapter F, Part 101, Subparts A and C, Federal Aviation Administration Regulations, or revisions or amendments thereto. Title 16, Code of Federal Regulations, Part 1500.85(8) and (9), Consumer Product Safety Commission Regulations. 2.3.2 Other Publications. Merriam-Webster s Collegiate Dictionary, 11th edition, Merriam-Webster, Inc., Springfield, MA, 2003. 2.4 References for Extracts in Mandatory Sections. NFPA 1125, Code for the Manufacture of Model Rocket and High Power Rocket Motors, 2012 2017 edition. NFPA 1127, Code for High Power Rocketry, 2013 2018 edition. Submitter Information Verification Submitter Full Name: Brian OConnor Organization: [ Not Specified ] Street Address: City: State: Zip: Submittal Date: Tue Sep 01 12:52:06 EDT 2015 Committee Statement Committee Statement: Updated references to most current editions
2 of 15 1/28/2016 11:48 AM Response Message: Ballot Results This item has passed ballot 30 Eligible Voters 5 Not Returned 24 Affirmative All 0 Affirmative with Comments 0 Negative with Comments 1 Abstention Not Returned Davidson, Randall W. A. Hill, Jr., Lansden E. Pier, David J. Rogers, John D. Wright, Darren Affirmative All Altland, Gregory S. Barber, III, Arthur H. Bowes, Richard Brown, Gary E. Cesaroni, Anthony J. Conkling, John A. Dean, Glenn A. Grucci, Phil Hanson, Garry Heckman, Julie L. Kaminski, Edward J. Lazarus, Joshua Lubliner, Stephen O'Lena, Mike Peart, Daniel P. Robbins, Rachel Roberts, Mary Rosenfield, Gary C. Steinberg, John R. Trout, Tad A. Weir, Christopher J. Wyman, Christopher T.
3 of 15 1/28/2016 11:48 AM Yarbrough, Marge Zmorenski, Tony Abstention Miller, John H. None.
4 of 15 1/28/2016 11:48 AM First Revision No. 10-NFPA 1122-2015 [ Section No. 4.2.3 ] 4.2.3 A model rocket motor shall be assembled with all pyrotechnic ingredients preloaded into a cylindrical paper or similarly constructed nonmetallic tube that does not fragment into sharp, hard pieces. Submitter Information Verification Submitter Full Name: Brian OConnor Organization: [ Not Specified ] Street Address: City: State: Zip: Submittal Date: Tue Aug 25 14:47:05 EDT 2015 Committee Statement Committee Statement: The deleted section conflicts with existing language that permits re-loadable motors. Response Message: Ballot Results This item has passed ballot 30 Eligible Voters 5 Not Returned 24 Affirmative All 0 Affirmative with Comments 0 Negative with Comments 1 Abstention Not Returned Davidson, Randall W. A. Hill, Jr., Lansden E. Pier, David J. Rogers, John D. Wright, Darren Affirmative All Altland, Gregory S. Barber, III, Arthur H. Bowes, Richard Brown, Gary E.
5 of 15 1/28/2016 11:48 AM Cesaroni, Anthony J. Conkling, John A. Dean, Glenn A. Grucci, Phil Hanson, Garry Heckman, Julie L. Kaminski, Edward J. Lazarus, Joshua Lubliner, Stephen O'Lena, Mike Peart, Daniel P. Robbins, Rachel Roberts, Mary Rosenfield, Gary C. Steinberg, John R. Trout, Tad A. Weir, Christopher J. Wyman, Christopher T. Yarbrough, Marge Zmorenski, Tony Abstention Miller, John H. None.
6 of 15 1/28/2016 11:48 AM First Revision No. 7-NFPA 1122-2015 [ Section No. 4.9.3 ] 4.9.3 As an alternative to the minimum launch site dimensions of Table 4.9, the size of the launch site shall be permitted to meet one of the following criteria: (1) It shall be not less than one-half the maximum altitude as stated by the manufacturer or as calculated by flight simulation for the model rocket and motor(s) combination being flown. (2) It shall be of a size approved by the AHJ based on flight demonstration or data required to substantiate the anticipated altitude. Submitter Information Verification Submitter Full Name: Brian OConnor Organization: [ Not Specified ] Street Address: City: State: Zip: Submittal Date: Tue Aug 25 13:46:12 EDT 2015 Committee Statement Committee Statement: Response Message: Many model rockets flown by consumers are original designs or are kits flown with types of motors not used by the manufacturer in listing the expected altitude that the rocket will attain. Some manufacturers do not list that expected altitude for their kits. In both cases, certain rockets can reach low altitudes with large rocket motors and can therefore be flown safely on a field smaller than the minimum dimensions prescribed in the table. Flight simulation computer programs are widely available both commercially and as downloadable freeware, and are widely used, which permit a consumer to accurately calculate the altitude that any rocket will attain with any motor. This proposed revision allows for use of that technique for developing an estimate of flight altitude for the purpose of informing minimum launch site dimensions. Public Input No. 19-NFPA 1122-2015 [Section No. 4.9.3] Ballot Results This item has passed ballot 30 Eligible Voters 5 Not Returned 24 Affirmative All 0 Affirmative with Comments 0 Negative with Comments 1 Abstention Not Returned
7 of 15 1/28/2016 11:48 AM Davidson, Randall W. A. Hill, Jr., Lansden E. Pier, David J. Rogers, John D. Wright, Darren Affirmative All Altland, Gregory S. Barber, III, Arthur H. Bowes, Richard Brown, Gary E. Cesaroni, Anthony J. Conkling, John A. Dean, Glenn A. Grucci, Phil Hanson, Garry Heckman, Julie L. Kaminski, Edward J. Lazarus, Joshua Lubliner, Stephen O'Lena, Mike Peart, Daniel P. Robbins, Rachel Roberts, Mary Rosenfield, Gary C. Steinberg, John R. Trout, Tad A. Weir, Christopher J. Wyman, Christopher T. Yarbrough, Marge Zmorenski, Tony Abstention Miller, John H. None.
8 of 15 1/28/2016 11:48 AM First Revision No. 8-NFPA 1122-2015 [ Section No. B.2 ]
9 of 15 1/28/2016 11:48 AM B.2 Code. The following text is excerpted from the Model Rocket Safety Code in its entirety. 1. Materials. I will use only lightweight, non-metal parts for the nose, body, and fins of my rocket. 2. Motors. I will use only certified, commercially-made model rocket motors, and will not tamper with these motors or use them for any purposes except those recommended by the manufacturer. 3. Ignition System. I will launch my rockets with an electrical launch system and electrical motor igniters. My launch system will have a safety interlock in series with the launch switch, and will use a launch switch that returns to the off position when released. 4. Misfires. If my rocket does not launch when I press the button of my electrical launch system, I will remove the launcher's safety interlock or disconnect its battery, and will wait 60 seconds after the last launch attempt before allowing anyone to approach the rocket. 5. Launch Safety. I will use a countdown before launch, and will ensure that everyone is paying attention and is a safe distance of at least 4.6 m (15 ft) away when I launch rockets with D motors or smaller, and 9.1 m (30 ft) when I launch larger rockets. If I am uncertain about the safety or stability of an untested rocket, I will check the stability before flight and will fly it only after warning spectators and clearing them away to a safe distance. When conducting a simultaneous launch of more than ten rockets I will observe a safe distance of 1.5 times the maximum expected altitude of any launched rocket. 6. Launcher. I will launch my rocket from a launch rod, tower, or rail that is pointed to within 30 degrees of the vertical to ensure that the rocket flies nearly straight up, and I will use a blast deflector to prevent the motor's exhaust from hitting the ground. To prevent accidental eye injury, I will place launchers so that the end of the launch rod is above eye level or will cap the end of the rod when it is not in use. 7. Size. My model rocket will not weigh more than 1500 g (53 oz) at liftoff and will not contain more than 125 g (4.4 oz) of propellant or 320 N-sec (71.9 lb-sec) of total impulse. If my model rocket weighs more than 453 g (1 lb) at lift-off or has more than 113 g (4 oz) of propellant, I will check and comply with Federal Aviation Administration regulations before flying. 8. Flight Safety. I will not launch my rocket at targets, into clouds, or near airplanes, and will not put any flammable or explosive payload in my rocket. 9. Launch Site. I will launch my rocket outdoors, in an open area at least as large as shown in Table B.2, and in safe weather conditions with wind speeds no greater than 32.22 km/h (20 mph). I will ensure that there is no dry grass close to the launch pad, and that the launch site does not present risk of grass fires. 10. Recovery System. I will use a recovery system such as a streamer or parachute in my rocket so that it returns safely and undamaged and can be flown again, and I will use only flame-resistant or fireproof recovery system wadding in my rocket. 11. Recovery Safety. I will not attempt to recover my rocket from power lines, tall trees, or other dangerous places. Table B.2 Launch Site Dimensions Installed Total Impulse (N-sec) Equivalent Motor Type Minimum Site Dimensions (ft) 0.00 1.25 1 4 A, 1 2 A 50 1.26 2.50 A 100 2.51 5.00 B 200 5.01 10.00 C 400 10.01 20.00 D 500 20.01 40.00 E 1000 40.01 80.00 F 1000 80.01 160.00 G 1000 160.01 320.00 2Gs 1500 Source: National Association of Rocketry. Supplemental Information
10 of 15 1/28/2016 11:48 AM File Name NAR_Model_Rocket_Safety_Code_Aug_2012_.1435450369944_1_.doc Description NAR Model Rocket Safety Code Submitter Information Verification Submitter Full Name: Brian OConnor Organization: [ Not Specified ] Street Address: City: State: Zip: Submittal Date: Tue Aug 25 13:49:58 EDT 2015 Committee Statement Committee Statement: Response Message: Appendix B contains a previous edition of the Model Rocket Safety Code of the National Association of Rocketry. This edition was superseded in August 2012 by a new edition, which has been attached. This new edition should be substituted in its entirety for the edition that is currently in Appendix B of NFPA 1122. Public Input No. 18-NFPA 1122-2015 [Section No. B.2] Ballot Results This item has passed ballot 30 Eligible Voters 5 Not Returned 24 Affirmative All 0 Affirmative with Comments 0 Negative with Comments 1 Abstention Not Returned Davidson, Randall W. A. Hill, Jr., Lansden E. Pier, David J. Rogers, John D. Wright, Darren Affirmative All Altland, Gregory S. Barber, III, Arthur H. Bowes, Richard Brown, Gary E. Cesaroni, Anthony J.
11 of 15 1/28/2016 11:48 AM Conkling, John A. Dean, Glenn A. Grucci, Phil Hanson, Garry Heckman, Julie L. Kaminski, Edward J. Lazarus, Joshua Lubliner, Stephen O'Lena, Mike Peart, Daniel P. Robbins, Rachel Roberts, Mary Rosenfield, Gary C. Steinberg, John R. Trout, Tad A. Weir, Christopher J. Wyman, Christopher T. Yarbrough, Marge Zmorenski, Tony Abstention Miller, John H. None.
NAR Model Rocket Safety Code Effective August 2012 1. Materials. I will use only lightweight, non-metal parts for the nose, body, and fins of my rocket. 2. Motors. I will use only certified, commercially made model rocket motors, and will not tamper with these motors or use them for any purposes except those recommended by the manufacturer. 3. Ignition System. I will launch my rockets with an electrical launch system and electrical motor igniters. My launch system will have a safety interlock in series with the launch switch, and will use a launch switch that returns to the "off" position when released. 4. Misfires. If my rocket does not launch when I press the button of my electrical launch system, I will remove the launcher's safety interlock or disconnect its battery, and will wait 60 seconds after the last launch attempt before allowing anyone to approach the rocket. 5. Launch Safety. I will use a countdown before launch, and will ensure that everyone is paying attention and is a safe distance of at least 15 feet away when I launch rockets with D motors or smaller, and 30 feet when I launch larger rockets. If I am uncertain about the safety or stability of an untested rocket, I will check the stability before flight and will fly it only after warning spectators and clearing them away to a safe distance. When conducting a simultaneous launch of more than ten rockets I will observe a safe distance of 1.5 times the maximum expected altitude of any launched rocket. 6. Launcher. I will launch my rocket from a launch rod, tower, or rail that is pointed to within 30 degrees of the vertical to ensure that the rocket flies nearly straight up, and I will use a blast deflector to prevent the motor's exhaust from hitting the ground. To prevent accidental eye injury, I will place launchers so that the end of the launch rod is above eye level or will cap the end of the rod when it is not in use. 7. Size. My model rocket will not weigh more than 1,500 grams (53 ounces) at liftoff and will not contain more than 125 grams (4.4 ounces) of propellant or 320 N-sec (71.9 pound-seconds) of total impulse. 8. Flight Safety. I will not launch my rocket at targets, into clouds, or near airplanes, and will not put any flammable or explosive payload in my rocket. 9. Launch Site. I will launch my rocket outdoors, in an open area at least as large as shown in the accompanying table, and in safe weather conditions with wind speeds no greater than 20 miles per hour. I will ensure that there is no dry grass close to the launch pad, and that the launch site does not present risk of grass fires.
10. Recovery System. I will use a recovery system such as a streamer or parachute in my rocket so that it returns safely and undamaged and can be flown again, and I will use only flame-resistant or fireproof recovery system wadding in my rocket. 11. Recovery Safety. I will not attempt to recover my rocket from power lines, tall trees, or other dangerous places. LAUNCH SITE DIMENSIONS Installed Total Impulse (N-sec) Equivalent Motor Type Minimum Site Dimensions (ft.) 0.00--1.25 1/4A, 1/2A 50 1.26--2.50 A 100 2.51--5.00 B 200 5.01--10.00 C 400 10.01--20.00 D 500 20.01--40.00 E 1,000 40.01--80.00 F 1,000 80.01--160.00 G 1,000 160.01--320.00 Two Gs 1,500
12 of 15 1/28/2016 11:48 AM First Revision No. 9-NFPA 1122-2015 [ Section No. E.1.2.1 ] E.1.2.1 NAR Publications. National Association of Rocketry, P.O. Box 407, Marion, IA 52302. Model Rocket Safety Code, 2001 August 2012. Submitter Information Verification Submitter Full Name: Brian OConnor Organization: [ Not Specified ] Street Address: City: State: Zip: Submittal Date: Tue Aug 25 13:51:36 EDT 2015 Committee Statement Committee Statement: Referenced current edition. Response Message: Public Input No. 2-NFPA 1122-2014 [Section No. E.1.2.1] Ballot Results This item has passed ballot 30 Eligible Voters 5 Not Returned 24 Affirmative All 0 Affirmative with Comments 0 Negative with Comments 1 Abstention Not Returned Davidson, Randall W. A. Hill, Jr., Lansden E. Pier, David J. Rogers, John D. Wright, Darren Affirmative All Altland, Gregory S. Barber, III, Arthur H.
13 of 15 1/28/2016 11:48 AM Bowes, Richard Brown, Gary E. Cesaroni, Anthony J. Conkling, John A. Dean, Glenn A. Grucci, Phil Hanson, Garry Heckman, Julie L. Kaminski, Edward J. Lazarus, Joshua Lubliner, Stephen O'Lena, Mike Peart, Daniel P. Robbins, Rachel Roberts, Mary Rosenfield, Gary C. Steinberg, John R. Trout, Tad A. Weir, Christopher J. Wyman, Christopher T. Yarbrough, Marge Zmorenski, Tony Abstention Miller, John H. None.
14 of 15 1/28/2016 11:48 AM First Revision No. 1-NFPA 1122-2015 [ Section No. E.2.2 ] E.2.2 TRA Publications. Tripoli Rocketry Association, Inc., P.O. Box 970010 87, Orem Bellevue, UT 84097 NE 68005. Comprehensive CAR/NAR/TRA Rocket Motor Certification List. Submitter Information Verification Submitter Full Name: Brian OConnor Organization: [ Not Specified ] Street Address: City: State: Zip: Submittal Date: Wed Aug 12 10:17:45 EDT 2015 Committee Statement Committee Statement: Updated to current location Response Message: Ballot Results This item has passed ballot 30 Eligible Voters 5 Not Returned 24 Affirmative All 0 Affirmative with Comments 0 Negative with Comments 1 Abstention Not Returned Davidson, Randall W. A. Hill, Jr., Lansden E. Pier, David J. Rogers, John D. Wright, Darren Affirmative All Altland, Gregory S. Barber, III, Arthur H. Bowes, Richard
15 of 15 1/28/2016 11:48 AM Brown, Gary E. Cesaroni, Anthony J. Conkling, John A. Dean, Glenn A. Grucci, Phil Hanson, Garry Heckman, Julie L. Kaminski, Edward J. Lazarus, Joshua Lubliner, Stephen O'Lena, Mike Peart, Daniel P. Robbins, Rachel Roberts, Mary Rosenfield, Gary C. Steinberg, John R. Trout, Tad A. Weir, Christopher J. Wyman, Christopher T. Yarbrough, Marge Zmorenski, Tony Abstention Miller, John H. None.