If somebody has a min diameter rocket for example and wants to use a CTI motor without an motor ejection charge for electronic deployment charge only for cases where Apogee happens way after the maximum delay length and a motor eject backup is impractical. What steps to remove the stock ejection charge from a CTI product? What steps to put dog barf where? Pictures please. With AT motors we simply don’t include the powder and I am familiar with that process for AT not for CTI. Thanks.