My late father, (who always watched 'The Dambusters' movie) served with 617. The Bomb rotated clockwise toward the rear of the aircraft. The greatest loss of stability was the start of the rotation, hence the run up which allowed the aircraft, as CVAIRWERKS rightly observed, time to settle. The effect was the aircraft would drop as the mass started its spin, which at 60 feet was not a lot of room, so the start-up was tried several ways; with the bomb rotating slowly initially so there was a lower inertial mass effect and also with it rotating all the way through the flight, then only coming up to 500rpm on the approach to target, but most methods put greater loading and strain on the components, particularly the motor, which was difficult to control and regulate the speed. In the end, the 10 minute run in was decided as best to allow adjustments. The aircraft did not fly at drop height all the way , but it was also suggested, to give clearance over trees, to pick a spot over fields to start the bomb, (seriously!) then allow the aircraft to stablise and drop back down to 60ft for run-in. The greatest danger was turning with the bomb spinning, the gyro effect was a real problem and only flying straight and level was the safest. It is certain a couple of aircraft, certainly P-Popsy which overshot and tried to turn out from the hills surrounding the dam, were caught out by this. Also the loss of engine power suddenly, such as knocked out by AA fire, would, at 60 feet, be a disaster, because again the gyro effect would temporarily cause loss of control of the aircraft. You have to remember that Wallis experimented and did most of his research with a spherical bomb initially, then moved to a shape resembling a edam cheese, with rounded edges. It was the cost of reinforcing the bomb led to reverting to a cylinder shape which was easier to assemble and install without special trusses to facilitate launch.