| 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) |
| Drogue |
|
| Main parachutes |
|
Deployment method
& charge |
|
Electronics
(if more than one device, list brand and model of each) |
|
| Initial Thrust |
(lbs) |
| Thrust to weight
ratio |
|
| Additional details or Links: |
|
|
| |
Number of motors |
Manufacturer
(or EX mfgr.) |
Designation (e.g., N2000) and delay |
Propellant Weight |
Total Impulse N-s |
|
Main Motor(s) |
|
|
|
|
|
|
Airstarts |
|
|
|
|
|
|
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 |
|
|
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) |
RockSim |
|
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) |
|
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