Reliant Robin
Formula
Chemical | Percentage |
---|---|
AP 400 | 35.00% |
AP 90 | 35.00% |
Al 5 | 12.00% |
Oxamide 4 | 1.00% |
R-45HTLO (Eq. Wt. 1234) | 11.13% |
HX-878 Tepanol | 0.30% |
Lecithin | 0.20% |
CAO-5 | 0.10% |
IDP | 3.34% |
MDI (Eq. Wt. 185) | 1.93% |
PDMS | 1 drop / 500 g propellant |
Burn Characteristics
Characteristic | Value |
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ISP |
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a | 0.0135 in/s |
n | 0.412 |
Density |
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Gamma |
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Molar mass | 24.98 g/mol |
C* | 5072 ft/s |
Chamber temperature | 2977 K @ 1000 psi |
Specific heat ratio | 1.198 |
Mixing Procedure
Step | Action |
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1 |
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2 |
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Pouring Procedure
Step | Action |
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1 |
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2 |
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Mixing Spreed Sheet
Mixing Log
Mixing Date | Serial Numbers | Site | Result |
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Motor Log
Identifier | Date | Site | Result |
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Notes
Reliant Robin is our high efficiency pourable propellant. It has been successfully run to Kn 550 at 1500 psi with no problems, making it tame and easy to work with. Due to the 5 μm aluminum, it combusts its metals easily with over 95% combusted in a 54mm 3 grain sized motor. Process it at about 80-90 °F for best pot life and pourability.
Pictures
Links
https://breakingballistics.weebly.com/reliant_robin.html
https://drive.google.com/drive/folders/17KeaGJN1kM-8gSaiOOhMAMA76fo6K0xS