ILoveRocket
New Member
Hi, I ran an open rocket simulation using Richard Nakka's spreadsheet. The value was set in data and kn and the value was output throughout tap. And I entered that value into the engine editor and transferred the information to the open rocket. However, the simulation showed an apogee of 1290 meters. But since I only used about 80 grams of fuel, that's not possible. I can't find where it went wrong. Please find the problem.