Loki Research
Motor Manufacturer
- Joined
- Aug 20, 2011
- Messages
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Hopefully I do this poll right. It's only the 2nd time I've ever done one. It's not something I'm currently working on, but when I do, I'd like to have this answered.
If I were to certify Loki Blue in the 54/2800 case, which of these two criteria would be more important to you?
1) Having the most possible total impulse with a little longer burn and a longer tail off of thrust.
2) Having a slightly lower total impulse but with higher average thrust/shorter burn and a quick/clean shut down with little to no tail off of thrust.
The best reason I can think of wanting #2 is for those who would prefer a booster motor with a fast clean shut down for a smooth quick separation.
I don't think that the number of those people wanting a booster motor would be very many, but I'm doing this to find out, just in case.
#1 could have around 3,500Ns and might be around an L~1630 with a 2.15 second burn.
#2 could have around as 3,300Ns and might be around an L~2000 with a 1.65 second burn.
#2 is a bit more difficult since the motor is a bit erosive and it's in its nature to have a bit of a tail off. More testing would need to be done to adjust the core size properly in order to eliminate the tail off of thrust. I'm just curious what people think.
Thank you,
If I were to certify Loki Blue in the 54/2800 case, which of these two criteria would be more important to you?
1) Having the most possible total impulse with a little longer burn and a longer tail off of thrust.
2) Having a slightly lower total impulse but with higher average thrust/shorter burn and a quick/clean shut down with little to no tail off of thrust.
The best reason I can think of wanting #2 is for those who would prefer a booster motor with a fast clean shut down for a smooth quick separation.
I don't think that the number of those people wanting a booster motor would be very many, but I'm doing this to find out, just in case.
#1 could have around 3,500Ns and might be around an L~1630 with a 2.15 second burn.
#2 could have around as 3,300Ns and might be around an L~2000 with a 1.65 second burn.
#2 is a bit more difficult since the motor is a bit erosive and it's in its nature to have a bit of a tail off. More testing would need to be done to adjust the core size properly in order to eliminate the tail off of thrust. I'm just curious what people think.
Thank you,
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