PolandBall
New Member
- Joined
- Nov 1, 2016
- Messages
- 1
- Reaction score
- 0
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
Time data
Competition settings
Competition conditions are not in use for this simulation.
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.
- 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 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
- 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
Time data
- Time to burnout: 1.809 Sec.
- Time to apogee: 8.229 Sec.
- Optimal ejection delay: 6.420 Sec.
Competition settings
Competition conditions are not in use for this simulation.