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TRIPOLI
HIGH-POWER ROCKETRY The following are Certification requirements for members of the Tripoli Rocketry Association, Inc. These were approved by the Tripoli Board of Directors in 2008 and in affect as of January 1st, 2009. LEVEL
1 Airframe – The rocket must be built by the flyer. The rocket shall have a display on the exterior identifying the calculated center of pressure. The rocket must be of “conventional rocket design”. “Odd Rockets” including flying pyramids, saucers and flying spools will not be allowed for any certification flight. The rocket may be either a kit or scratch built. Scratch built rockets may contain commercially built components Recovery - Standard parachute recovery is required. Non-parachute recovery methods (e.g. tumble, helicopter, gliding, etc) are not permitted for certification flights. If the rocket is using dual deployment, the first event recovery can be via drogue-less or streamer as long as the main or second event uses a standard parachute. Motor – The certification flight must be with a single certified H or I motor (tested total impulse between 160.01 and 640.00 n-sec). Staged and/or Clustered rockets may not be used for certification flights. The flyer shall be observed by the certifying member or their designated representative during the assembly (if a reload or hybrid) and preparation of the motor. Electronics – Electronics are not required for level 1 certification flights. Certification Flight – Level 1 Certification flight may take place at any insured launch. The certifying member (i.e. Prefect, TRA Director, or TAP Member) must be present and witness the certification flight. The certifying member must witness the rocket ascend in a stable manner and descend in stabilized manner controlled by the recovery system. Post-Flight Inspection – The rocket must be presented to the certifying member for inspection. If the rocket cannot be recovered, but can be inspected in place (power lines, tree, etc…) this is acceptable. The certifying member shall inspect the rocket for excessive damage. Excessive damage shall be considered damage to the point that if the flyer were handed another motor, the rocket could not be put on the pad and flow again safely. Damage caused by wind dragging will not cause a disqualification. Non-certification – Any of the following will result in non-certification for a certification flight:
LEVEL
2 Written Test – The written examination for level 2 shall be passed prior to a level 2 certification flight. Airframe – The rocket must be built by the flyer. The rocket shall have a display on the exterior identifying the calculated center of pressure. The rocket must be of “conventional rocket design”. “Odd Rockets” including flying pyramids, saucers and flying spools will not be allowed for any certification flight. The rocket may be either a kit or scratch built. Scratch built rockets may contain commercially built components. Recovery - Standard parachute recovery is required. Non-parachute recovery methods (e.g. tumble, helicopter, gliding, etc) are not permitted for certification flights. If the rocket is using dual deployment, the first event recovery can be via drogue-less or streamer as long as the main or second event uses a standard parachute. Motor – The certification flight must be with a single certified J, K, or L motor (tested total impulse between 640.01 and 5120.00 n-secs). Staged and/or Clustered rockets may not be used for certification flights. The flyer shall be observed by the certifying member or their designated representative during the assembly (if a reload or hybrid) and preparation of the motor. Electronics – Electronics are not required for level 2 certification flights. However, prior to attempting level 3 certification, the flyer shall successfully fly at least one rocket in the Level 2 impulse range using an electronic device as the primary means of recovery system deployment. This may be their level 2 certification flight or any subsequent flight. Certification Flight – Level 2 Certification flight may take place at any insured launch. The certifying member (i.e. Prefect, TRA Director, or TAP Member) must be present and witness the certification flight. The certifying member must witness the rocket ascend in a stable manner and descend in stabilized manner controlled by the recovery system. Post-Flight Inspection – The rocket must be presented to the certifying member for inspection. If the rocket cannot be recovered, but can be inspected in place (power lines, tree, etc…) this is acceptable. The certifying member shall inspect the rocket for excessive damage. Excessive damage shall be considered damage to the point that if the flyer were handed another motor, the rocket could not be put on the pad and flow again safely. Damage caused by wind dragging will not cause a disqualification. Non-certification – Any of the following will result in non-certification for a certification flight:
LEVEL
3 Airframe – The rocket must be built by the flyer. The rocket shall have a display on the exterior identifying the calculated center of pressure. The rocket must be of “conventional rocket design”. “Odd Rockets” including flying pyramids, saucers and flying spools will not be allowed for any certification flight. The rocket may be either a kit or scratch built. Scratch built rockets may contain commercially built components. Commercially available prefabricated fin cans, either as part of a kit or obtained separately, may not be used for level 3 certification flights. Construction Inspections - TRA members designing or preparing to fly a level 3 project must present details of their design to 2 TAP members of their choice. BEFORE attempting a level 3 flight, 2 TAP members must have signed off on the member’s certification form. It is best if this TAP review is performed before the day of the launch to allow adjustments to the rocket design if deemed necessary by either of the 2 TAP reviewers. TAP members should be kept informed of any changes during construction. In general, the TAP member for objectively assessing the rocket will need the following information:
Recovery - Standard parachute recovery is required. Non-parachute recovery methods (e.g. tumble, helicopter, gliding, etc) are not permitted for certification flights. If the rocket is using dual deployment, the first event recovery can be via drogue-less or streamer as long as the main or second event uses a standard parachute. Motor – The certification flight must be with a single certified M or larger motor (tested total impulse greater than 5120.01 n-secs). Staged and/or Clustered rockets may not be used for certification flights. The flyer shall be observed by the TAP member or their designated representative during the assembly (if a reload or hybrid) and preparation of the motor. Electronics – Prior to a level 3 certification flight, the flyer shall successfully fly at least one rocket in the level 2 range using an electronic device as the primary means of recovery system deployment. Level 3 certification flights shall include at least two completely separate electronic devices, with independent power sources, wire harnesses, and ignition devices for the primary and back-up means of recovery system deployment. Certification Flight – Level 3 Certification flight may take place at any insured launch. The TAP member must be present and witness the certification flight. The TAP member must witness the rocket ascend in a stable manner and descend in stabilized manner controlled by the recovery system. Post-Flight Inspection – The rocket must be presented to the certifying member for inspection. If the rocket cannot be recovered, but can be inspected in place (power lines, tree, etc…) this is acceptable. The certifying member shall inspect the rocket for excessive damage. Excessive damage shall be considered damage to the point that if the flyer were handed another motor, the rocket could not be put on the pad and flow again safely. Damage caused by wind dragging will not cause a disqualification. Non-certification – Any of the following will result in non-certification for a certification flight:
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