High Altitude Project
Submission Form
During ARLISS/XPRS 2017 the military wants to do some training with GPS jamming so they don't want us to encroach on their MOA. So no high flights (above 60k) for us until next year

Submission must be 30 days in advance of launch

Launch Day: [ 1 ] [ 2 ] [ 3]
Launch window: [ 6:00-10:00]  [ 10:00-14:00]  [ 14:00-18:00]
Primary Contact Name:
Primary Contact Email:
Affiliated Club:
Flyers' Names, addresses, TRA numbers and Levels.

(all must be in good standing)

Project / Rocket Name:
Kit name: (or scratch built)
Project's Web Page: (if applicable)
If not a kit, describe the rocket briefly (3 FNC, scale model, upscale from kit, important features, color scheme, etc.)
Total Length   (feet / inches)
Diameter   (inches)
Weight without motors   (lbs)
Weight with Motors   (lbs)
Main parachutes
Deployment method & charge
Estimated Recovery Area
(if more than one device, list brand and model of each)
Please specify any special frequency (telemetry or otherwise) that you might need reserved for your flight.
Initial Thrust (lbs)
Thrust to weight ratio
Additional details or Links:


Number of motors

(or EX mfgr.)

Designation (e.g., N2000) and delay

Propellant Weight

Total Impulse N-s

Main Motor(s)
Second stage
Third stage
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.  For larger motors, a printout from a motor modeling program is expected.  Additional information (casing wall thickness, specific propellant formulation, etc.) is also expected for such motors. 

Rail/Rod; length, other launch system details
Will you need a ladder or any other non-standard equipment to be provided?
Motor ignition description and sequence (if applicable)

Simulation Data:  Results from (data should be included from each program or simulation actually used)

Simulation estimate based on (one is required, two are better)


Cd (coefficient of drag)

Stability margin (calibers of stability)
Velocity (ft/s): At top of launcher
Maximum Velocity
Maximum altitude (ft)
Will staging occur at or greater than Mach 1.0? (Y/N/not applicable)
Attach file:   (if multiple, please .ZIP into one file)
File description

Submission must be 30 days in advance of launch.



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