>Did anyone else notice that the calculated flap servo torque requirement (62 >in-oz) is higher than the specs on all commonly used servos other than the >Volz Micro Maxx HP. The JR DS368 is spec'ed at 53 oz-in. The thin wing >servos, JR DS-168 and Hitec equivalent at 46.6 oz-in.
Two comments: 1) What Daryl said. The assumed 200 lb load is kinda huge. 2) If the flaps and ailerons don't move significantly during the last few seconds before the zoom where the load maximizes, then the torque requirements I quoted are for holding torque, not working torque. AFAIK, digital servos like the DS368 have way more holding torque than their spec'd torque. In that case they should be OK for the flaps. RCSE-List facilities provided by Model Airplane News. Send "subscribe" and "unsubscribe" requests to [EMAIL PROTECTED] Please note that subscribe and unsubscribe messages must be sent in text only format with MIME turned off. Email sent from web based email such as Hotmail and AOL are generally NOT in text format
