Loki Research
Motor Manufacturer
- Joined
- Aug 20, 2011
- Messages
- 1,409
- Reaction score
- 596
I have been meaning to mention this about Loki Research motors for some time now. I came across a thread showing a photo of the assorted parts of an AT J-510 motor. One comment asked what all the small o-rings were for. If this were a CTI motor, it might have been more obvious since they are much more common with that product line.
Well at Loki Research, I started to go down that path at one point and I even bagged a few 54mm reloads at one time with them. In the end, Loki Research does not use o-ring grain spacers on any reloads. I do something that I feel is better.
Grain spacer o-rings are very thin, and at least on snap ring sizes in 54mm, I've had more than a few that wanted to roll up between the grain and the liner which results in a stuck grain. They also take away 1/16" of propellant space for every o-ring used. Call me stingy, nit-picky, whatever, but I'd rather put propellant in a motor rather than empty space. Sure, the performance loss isn't great, but high performance and low cost was always one of the things Loki Research set out to deliver back in 2004-2005.
So instead of using o-rings, here's what I do. Every grain at Loki Research from the 38/1200 and up is cast and cut by me, by hand. The only slightly automated process is done in the mixing of the propellant and the cutting of the 38/120 thru 740Ns grains. Since these are all "hand made" reloads, it is quite easy for me to take a little more time and cut a chamfer into the face of each propellant grain. The loss is about 1 gram of propellant for this sliver thin slice, but honestly I'd have to go back and look if that was in 54mm or 76mm. I'm pretty certain that was the weight taken from these 54mm grains. 1/16" of propellant is about 4 grams. So 4 grains, 8 faces for this reload would equal 32g of propellant loss (~64Ns) for o-rings, or 8g of propellant loss (16Ns) for cutting in chamfers.
Pictured below are 4 grains from the 54/2800 red reload that is awaiting testing certification. There is a1/4" wide phenolic flat edge running across the center of all 4 grains with a bright light held behind them so you can somewhat see the chamfer in the grain faces. It was rather hard to get the camera to capture this as good as the eye can, and the 1/4" wide flat edge hides more of the light at the OD of the grains. Only a tiny gap is needed for the flame front to reach the surface of the grain faces, and this is only showing one of two sides. Mate two of these together and you have plenty of a gap for fast, complete ignition, but with about 1/4 the loss of propellant and Ns over using o-rings. On this size motor with around 3,300Ns and 1,684g of propellant, that's a 2% loss loss compared to a .5% loss. To me, every little bit counts.
Not having grains spacer mean there are several less o-rings for you to worry about doing the right/wrong thing with. It means a slight performance edge, and in the case of Loki Research, it means you have a hand made, custom reload that will be a joy to assemble and awesome to watch fly.
Thank you,
Well at Loki Research, I started to go down that path at one point and I even bagged a few 54mm reloads at one time with them. In the end, Loki Research does not use o-ring grain spacers on any reloads. I do something that I feel is better.
Grain spacer o-rings are very thin, and at least on snap ring sizes in 54mm, I've had more than a few that wanted to roll up between the grain and the liner which results in a stuck grain. They also take away 1/16" of propellant space for every o-ring used. Call me stingy, nit-picky, whatever, but I'd rather put propellant in a motor rather than empty space. Sure, the performance loss isn't great, but high performance and low cost was always one of the things Loki Research set out to deliver back in 2004-2005.
So instead of using o-rings, here's what I do. Every grain at Loki Research from the 38/1200 and up is cast and cut by me, by hand. The only slightly automated process is done in the mixing of the propellant and the cutting of the 38/120 thru 740Ns grains. Since these are all "hand made" reloads, it is quite easy for me to take a little more time and cut a chamfer into the face of each propellant grain. The loss is about 1 gram of propellant for this sliver thin slice, but honestly I'd have to go back and look if that was in 54mm or 76mm. I'm pretty certain that was the weight taken from these 54mm grains. 1/16" of propellant is about 4 grams. So 4 grains, 8 faces for this reload would equal 32g of propellant loss (~64Ns) for o-rings, or 8g of propellant loss (16Ns) for cutting in chamfers.
Pictured below are 4 grains from the 54/2800 red reload that is awaiting testing certification. There is a1/4" wide phenolic flat edge running across the center of all 4 grains with a bright light held behind them so you can somewhat see the chamfer in the grain faces. It was rather hard to get the camera to capture this as good as the eye can, and the 1/4" wide flat edge hides more of the light at the OD of the grains. Only a tiny gap is needed for the flame front to reach the surface of the grain faces, and this is only showing one of two sides. Mate two of these together and you have plenty of a gap for fast, complete ignition, but with about 1/4 the loss of propellant and Ns over using o-rings. On this size motor with around 3,300Ns and 1,684g of propellant, that's a 2% loss loss compared to a .5% loss. To me, every little bit counts.
Not having grains spacer mean there are several less o-rings for you to worry about doing the right/wrong thing with. It means a slight performance edge, and in the case of Loki Research, it means you have a hand made, custom reload that will be a joy to assemble and awesome to watch fly.
Thank you,