From 557f233a4474d20b87760499970ce618588d680b Mon Sep 17 00:00:00 2001
From: Bdale Garbee
Date: Wed, 31 May 2017 21:00:46 -0600
Subject: [PATCH] move simulation results up before Results heading
---
rockets/research/2017-batch-03.mdwn | 12 ++++++------
1 file changed, 6 insertions(+), 6 deletions(-)
diff --git a/rockets/research/2017-batch-03.mdwn b/rockets/research/2017-batch-03.mdwn
index 00da1b0..49d89ac 100755
--- a/rockets/research/2017-batch-03.mdwn
+++ b/rockets/research/2017-batch-03.mdwn
@@ -14,7 +14,12 @@ increased during melting to 300F indicated.
These grains were cast on 31 May 2017.
-Liner should be cut to 10.00" long for this 6-grain reload.
+Liner should be cut to 10.00" long for this 6-grain reload. Simulation says:
+
+
+29mm 6-grain Erythritol #14 |
---|
Rating: | 43% H-162 | Max Pressure: | 5.92 MPa (859 psi) |
---|
Total Impulse: | 216 Ns | Specific Impulse: | 133 s |
---|
Max Thrust: | 206 N | Volume Loading: | 70% |
---|
Average Thrust: | 162 N | Fuel Mass: | 165 g |
---|
|
+
+
## Results ##
@@ -30,8 +35,3 @@ Average casting tube mass 1.13g.
With a 10.00" liner, 14/64" nozzle throat, buna-n o-rings, simulation says
this makes a 37% H-156, 208 Ns, with about a 1.2 sec burn.
-
-29mm 6-grain Erythritol #14 |
---|
Rating: | 43% H-162 | Max Pressure: | 5.92 MPa (859 psi) |
---|
Total Impulse: | 216 Ns | Specific Impulse: | 133 s |
---|
Max Thrust: | 206 N | Volume Loading: | 70% |
---|
Average Thrust: | 162 N | Fuel Mass: | 165 g |
---|
|
-
-
-
--
2.30.2