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Launch of the rocket Globos, (embedded subtitle)
AIRrocketry
459 views
Press coverage from Channel 2 about the Globos launch.
This rocket was powered by KNER propellant to an altitude of 2.6 km (8500 feet). The maximum velocity was in the ...
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Launch of the rocket Globos
AIRrocketry
498 views
The Globos rocket was powered by KNER propellant to 2700 meters and 1000 km/h with an acceleration of 14 g. All aluminum body apart from the nose cone that was fabricated o...
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Parachute Ejection Test
AIRrocketry
596 views
Parachute ejection using a 16 g CO2 cartridge and the Rouse Tech system. TAC-1 60" chute from giantleap rocketry.
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Third static test of the AIRKNER flight motor - View 3
AIRrocketry
214 views
Good and rapid built up and the best burn yet. The motor is "safe to launch"
Total impulse somewhere around 2700 Ns with a maximum thrust of 1100 N and maximum chamber pre...
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Third static test of the AIRKNER flight motor - View 1
AIRrocketry
191 views
Good and rapid built up and the best burn yet. The motor is "safe to launch"
Total impulse somewhere around 2700 Ns with a maximum thrust of 1100 N and maximum chamber pre...
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Third static test of the AIRKNER flight motor - View 2
AIRrocketry
187 views
Good and rapid built up and the best burn yet. The motor is "safe to launch"
Total impulse somewhere around 2700 Ns with a maximum thrust of 1100 N and maximum chamber pre...
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Second static test of the AIRKNER flight motor - View 3
AIRrocketry
141 views
Good test, the ignition problem was solved and we got a nice and rapid built up. Total impulse somewhere around 2700 Ns with a maximum thrust of 1100 N and maximum chamber ...
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Second static test of the AIRKNER flight motor - View 2
AIRrocketry
131 views
Good test, the ignition problem was solved and we got a nice and rapid built up. Total impulse somewhere around 2700 Ns with a maximum thrust of 1100 N and maximum chamber ...
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Second static test of the AIRKNER flight motor - View 1
AIRrocketry
176 views
Good test, the ignition problem was solved and we got a nice and rapid built up. Total impulse somewhere around 2700 Ns with a maximum thrust of 1100 N and maximum chamber ...
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KNER Flight Motor Static Test - View3
AIRrocketry
165 views
9 Bates Grain of KNER (65/35) Propellant
2.1 kg in total
50 mm Diameter
20 mm Core
85 mm in Length
Max thrust: 900N
Max Chamber Pressure: 35 bars
Good test despite the del...
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