| Subject: Comprehensive Cooling summation. |
| From: Paul |
| Date: 9/25/1999, 7:26 PM |
| To: zz |
X-Mozilla-Keys: Jim Mosur wrote:
Hi Paul I have been monitoring my coolant return from rads to engine. Coolant to rads 187 F., coolant from rads. to engine 135-140 F. Hard climb temps are 5-8 degrees higher. Jim Mosur RV6 13B
BTW Jim, what are your gross weight and climb numbers? Paul Lamar The Aircraft Rotary Engine Newsletter. Powered by Linux. http://home.earthlink.net/~rotaryeng/ http://www.linux.org