Look at the potential failure modes in a typical fully redundant ejection system versus the one you proposed:
Fully redundant system:
Altimeter 1
Battery 1
Ematch 1
Charge 1
Altimeter 2
Battery 2
Ematch 2
Charge 2
A failure of one or more components in system 1 has no effect on system 2 and vice versa. The probability of a failure of any component is low, but not zero. For the rocket to have no deployment requires BOTH systems have to fail. If either system works you will have a deployment if your charge is sufficient to deploy the recovery system.
Your proposed system:
Altimeter 1
Battery 1
Altimeter 2
Battery 2
Ematch
Charge
Let's assume there are no electrical issues with your proposed system.* If battery 1 or altimeter 1 fails, the system will still work if altimeter 2 and battery 2 work. The same is true if battery 2 or altimeter 2 fail, the system will still work if altimeter1 and battery 1 work. However, the entire system fails if the ematch or the charge fail. So, you have the extra weight of a second altimeter and battery and little of the benefits of a redundant system. A second charge and ematch add little weight and make the system fully redundant.
*In general you want to avoid sending a large current from one electronic device into another one. If you were to use a system like this, you would want to electrically isolate the two systems from each other.