High Altitude Project Submission

High Altitude Project Submission Form

50,000 feet (or higher)

The individual responsible for the flight is required to submit this form.
Submission must be made no later than 30 days before the start date of the Aeropac launch you plan to attend for your flight.
Submission of this form does not constitute approval.
You may be contacted for additional information.
You will be contacted once approval is granted.
If you are not contacted within 7 days prior to the flight, please contact Aeropac’s Webmaster.

Note: If the maximum altitude of your flight is expected to reach or exceed 100,000 feet, you must also obtain approval from the Tripoli Class 3 Committee. Regardless of expected altitude, any rocket with a motor or a combination of motors that exceed 40,960 Ns cannot be flown via the Aeropac FAA Waiver. All such rockets are Class 3 rockets and must be submitted to the Tripoli Class 3 committee for review and approval. The flier must obtain their own FAA Waiver. If a flier wishes to coordinate such a flight during an Aeropac launch, they should coordinate with the Prefect.

* denotes required fields

Project Information

Launch Launch Day Launch Window Responsible Individual Contact Name NAR / TRA number and certification level E-mail Address Affiliated Club Flyers' Names, addresses, TRA numbers and Levels

Rocket Details

Project / Rocket Name Kit name (or scratch built) Project's Web Page

Project Description

Total Length Diameter(s) Weight without motor(s) Weight with motor(s) Drogue chute / details Main chute(s) / details Deployment method and charges Estimated Recovery Area Electronic Details Special frequency (telemetry/otherwise) that you might need reserved for your flight Initial Thrust (lbs) Thrust to weight ratio Additional details or links

Main Motor(s)

Number of Motors Manufacturer Designation Delay Propellant Weight Total Impulse

Second Stage Motor(s)

Number of Motors Manufacturer Designation Delay Propellant Weight Total Impulse

Staging will occur at or greater than Mach 1.0.

Total Installed

Propellant Weight Impulse N-S

Describe each EX Motor

Diameter, designation (J200, etc.), type and number of grains, propellant description, anticipated pressure, etc. Motors of less than 10240 N-s may be described very briefly.

Launch Support Requirements

Rail/Rod; length, other launch system details

I will need a ladder at the pad.

I will need non-standard equipment to be provided.

Describe the non-standard equipment needed. Motor ignition description and sequence (if applicable)

Simulation Data

When you email your form, attach the results from any computer simulations you used. They must be included from each program actually used. Simulations are required using commercial or publicly available, off-the-shelf software, or equivalent.

Signature

All the supplied information is true and correct to the best of my knowledge. I acknowledge that I am responsible for the safe launch, flight and recovery of my rocket within the Aeropac waiver cylinder and altitude limits.