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Written by Administrator
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Aug 04, 2010 at 08:35 PM |
Initial Design (Exoge-6-4500N-40s)
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Exoge 6-4500N-40S |
| Engine | 4500N-40S |
| Engine Type | Hybrid |
| Oxidizer | Nitrous Oxide |
| Fuel | HDPE |
| Thrust | 4500N (1000 lbs) |
| Injector | Annular |
| Ignition | KN/Epoxy Solid |
| Pre/Post Burner | Graphite |
| Nozzle/Throat | Graphite |
| Isp | 210s |
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| Rocket | Exoge 6 |
| Diameter | 15.25cm (6 in) |
| Length | 5m (16.4 ft) |
This is our initial design for our sub orbital attempt. We will design and
test fire the engine first. We need to work on regression rates and get
the appropriate length to diameter for the fuel grain. Once the engine has
been thoroughly tested we plan on testing the electronic flight hardware.
We will first test it in HPR equipment from various vendors. The
electronics needs to be able to detect apogee, monitor atmospheric pressure,
track acceleration, track earths magnetic field, and communications. We
have a long road ahead of us but we feel we can achieve the goal.
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Last Updated ( Aug 30, 2010 at 07:29 PM )
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