- Jun 25, 2012
- Reaction score
Would like to use a Raven in a stubby two stage rocket to airstart the second stage and execute the apogee chute deployment in the second stage. Due to space limitations, the location of the Raven would have to be in the nosecone. As such, the barometer-based deployment function would probably be unreliable. Do you see any problem with relying on the accelerometer function detection of apogee for chute deployment? Could use the timer function also I suppose.