After taking a good, long, hard look at my rocketry goals, I've decided to move up my timetable and attempt to acquire a Level 1 certification in 2023. To that end, I have selected an airframe and various motors that I believe will be suitable for test and certification flights, based on information gleaned from online resources which include TRF. I intend to purchase the airframe kit on New Years' Day, which is just a few hours away as I post this. I'm practically jumping up and down with excitement, I finally get to pull the trigger on a lifetime goal!
My selection is the Enerjet by Aerotech Astrobee D, which I will assemble fully by the book at a leisurely pace, and attempt to get a really good-looking finish. I will then proceed with a rigorous flight test program on Enerjet by Aerotech F67-6W and G74-6W motors, which are recommended by Aerotech's 2021-2022 catalog. I also validated these motor selections in OpenRocket and ThrustCurve, with simulations set for both calm and severe winds (20mph). In both cases, the F67-6W is less than a second long, and the G74-6W is less than a second short. Both are predicted to stay under DART's 1000 ft ceiling. Rail departure speed, stability margin, thrust-to-weight ratio, and liftoff mass are all legal and good.
Should these flights go well and I'm left confident that I could recover the rocket on H power at a high-power site, I will get my paperwork in order, arrange for certification witnessing, and make a certification attempt on an AeroTech H115DM. Apogee's product page recommends a delay drilled to 9 seconds, which is corroborated by my findings in OpenRocket and ThrustCurve. Because the Universal Delay Drilling Tool drills in 2-second increments down from the 14 that the motor comes with, I'll probably be going for 10, as the simulations indicate that in calm winds, the optimum delay will be very slightly more than 9 seconds. Things were very dicey with severe winds, with the optimal delay time drifting wildly through the 8- to 9-second range as I ran the OpenRocket simulation multiple times, so the flight will have to be made in cooperative winds, I'd say no more than 5mph. I will plug in more precise data for my selected launch site's coordinates, elevation, and predicted atmospheric conditions when the time comes for a certification attempt.
This thread will document my progress through this plan, as well as all of the setbacks, delays, and rethinks that Imay will experience along the way. I'll get pictures where I can, and I will also try to get my hands on a suitable camera system to mount on the rocket, and capture the flights on video.
My selection is the Enerjet by Aerotech Astrobee D, which I will assemble fully by the book at a leisurely pace, and attempt to get a really good-looking finish. I will then proceed with a rigorous flight test program on Enerjet by Aerotech F67-6W and G74-6W motors, which are recommended by Aerotech's 2021-2022 catalog. I also validated these motor selections in OpenRocket and ThrustCurve, with simulations set for both calm and severe winds (20mph). In both cases, the F67-6W is less than a second long, and the G74-6W is less than a second short. Both are predicted to stay under DART's 1000 ft ceiling. Rail departure speed, stability margin, thrust-to-weight ratio, and liftoff mass are all legal and good.
Should these flights go well and I'm left confident that I could recover the rocket on H power at a high-power site, I will get my paperwork in order, arrange for certification witnessing, and make a certification attempt on an AeroTech H115DM. Apogee's product page recommends a delay drilled to 9 seconds, which is corroborated by my findings in OpenRocket and ThrustCurve. Because the Universal Delay Drilling Tool drills in 2-second increments down from the 14 that the motor comes with, I'll probably be going for 10, as the simulations indicate that in calm winds, the optimum delay will be very slightly more than 9 seconds. Things were very dicey with severe winds, with the optimal delay time drifting wildly through the 8- to 9-second range as I ran the OpenRocket simulation multiple times, so the flight will have to be made in cooperative winds, I'd say no more than 5mph. I will plug in more precise data for my selected launch site's coordinates, elevation, and predicted atmospheric conditions when the time comes for a certification attempt.
This thread will document my progress through this plan, as well as all of the setbacks, delays, and rethinks that I