LOC Norad Pro Maxx + Aerotech G80 137ns

[PolandBall]

Hi
I have norad pro kit, but no chance for certification in Poland, I want order aerotech G80-7T.
what you think about it? I want use 29/38 mma-2 adapter,
in the nose cone installing my old apm 2.6 with gps and radio modem 433mhz for live telemetry.
if its possible making deployment near transition tube.

Motor specs:

NEW (137 Ns) TYPE
Blue Thunder G80 motors with a 7 second delay.
Single use composite motors for 29mm motor mounts (Aerotech and other kits).
Includes molded-in thrust ring
Package includes 1 Motor and 1 igniter.
Length: 124 mm
Diameter: 29 mm
Weight: 128 gr
Max liftoff weight: 1474 gr


Simulation data (rocksim)
Including only model and motor weight


LOC Norad Pro Maxx - Simulation results
Engine selection
[G80T-7]
Simulation control parameters

• Flight resolution: 800.000000 samples/second
• Descent resolution: 1.000000 samples/second
• Method: 4th Order runge-kuta.
• End the simulation when the rocket reaches the ground.

Launch conditions

• Altitude: 0.00 m
• Relative humidity: 50.000 %
• Temperature: 15.000 Deg. C
• Pressure: 29.9139 In.
• Wind speed model: Calm (0-2 MPH)
  • Low wind speed: 0.0000 KPH
  • High wind speed: 3.2187 KPH
• Wind turbulence: Fairly constant speed (0.01)
  • Frequency: 0.010000 rad/second
• Wind starts at altitude: 0.00 m
• Launch guide angle: 15.000 Deg.
• Latitude: 0.000 Degrees

Launch guide data:

• Launch guide length: 140.000 cm
• Velocity at launch guide departure: 59.8245 KPH
• The launch guide was cleared at : 0.183 Seconds
• User specified minimum velocity for stable flight: 48.2796 KPH
• Minimum velocity for stable flight reached at: 92.919 cm

Max data values:

• Maximum acceleration:Vertical (y): 0.103 km/s/sHorizontal (x): 0.010 km/s/sMagnitude: 0.104 km/s/s
• Maximum velocity:Vertical (y): 402.8364 KPH, Horizontal (x): 42.0346 KPH, Magnitude: 405.0173 KPH
• Maximum range from launch site: 58.76 m
• Maximum altitude: 386.54 m

Recovery system data
Time data

• Time to burnout: 1.809 Sec.
• Time to apogee: 8.229 Sec.
• Optimal ejection delay: 6.420 Sec.

Landing data
Competition settings
Competition conditions are not in use for this simulation.

 

[watermelonman]

Seems like a good plan to me. Remember to compensate for the extra weight when you add more electronics and other payload.