# 57300 Motor Documentation [ToC] ## Overviews ![](https://hackmd.io/_uploads/HkI4k4DA3.png) ![](https://hackmd.io/_uploads/SkwpQVvA3.png) ### Revision #### V1 - Minimal design - Nozzle - Lid - Tube - Propellent ### Parameters - Peak Pressure: 1.89MPa - Total Impuse: 1264Ns - ISP: 110.24s - Classification: J - Peak Thrust: 370N ## Nozzle ![](https://hackmd.io/_uploads/r1zNVorC3.png) ### Parameters - Material: Stainless Steel - Throat Diameter: 14mm - Exit Diameter: 28mm - Convergence Half Angle: 60° - Divergence Half Angle: 15° - O-Ring: AS568-033 FKM - Fixed by 4 M4 12.9 metric coarse pitch thread ### Saftey Nozzle's Area $$ A = ((\frac{57mm}{2})^2\cdot\pi) - ((\frac{14mm}{2})^2\cdot\pi) = 2.3978 \times 10^{-3} m^2 $$ Force on the nozzle $$ F_{nozzle} = P \cdot A = 1.89MPa \cdot 2.3978 \times 10^{-3} m^2 = 4531.84N $$ #### Bolt Saftey Factor M4 12.9 Shear Proof Load $$ F_p = 8520N \\ F_{p\tau} = Fp \cdot 0.57 = 4856.4N $$ Using 4 M4 12.9 screws $$ SF = 4 \cdot F_{p\tau}/F_{nozzle} = 19425.6N/4531.84N = 4.28 $$ ## Lid ### Parameters - Material: Stainless Steel - Thickness: 15mm - Diameter: 57mm - O-Ring: AS568-033 FKM - Fixed by 5 M4 12.9 metric coarse pitch thread ### Saftey Lid's Area $$ A = ((\frac{57mm}{2})^2\cdot\pi) = 2.5517 \times 10^{-3} m^2 $$ Force on the lid $$ F_{lid} = P \cdot A = 1.89MPa \cdot 2.5517 \times 10^{-3} m^2 = 4822.71N $$ #### Bolt Saftey Factor M4 12.9 Shear Proof Load $$ F_p = 8520N \\ F_{p\tau} = Fp \cdot 0.57 = 4856.4N $$ Using 5 M4 12.9 screws $$ SF = 5 \cdot F_{p\tau}/F_{lid} = 24282N/4822.71N = 5.03 $$ ## Tube ### Parameters - Material: 6061 aluminum alloy tube - Tube Length: 300mm** - Burning Grain Length: 300mm - Thickness: 3.15mm - Inside Diameter: 57.2mm - Outside Diameter: 63.5mm ### Saftey #### Barlow's formula $$ P = \frac{2\sigma_{\theta} s}{D} $$ - $P$ Internal Pressure - $\sigma_{\theta}$ Allowable stress - $s$ Wall thickness - $D$ Outside diameter #### Saftey Factor 6061 aluminum alloy 3mm thick tube has yield tensile strength $F_{ty}=16ksi\approx 110.31MPa$ $$ P = \frac{2 \cdot 110.31MPa \cdot 3.15mm}{63.5mm} = 10.94MPa $$ $$ SF = P / P_{peak} = 10.94MPa/1.89MPa = 5.78 $$ ## Grains ![](https://hackmd.io/_uploads/S1RVZsHAh.png) ### Parameters (Pre Grain) - Propellant: KNSB (65wt% KNO3 35wt% sorbitol) - Port Diameter: 20mm - Port Offset: 18mm - Segment Length: 150mm - Quantity of grain: 2 - Total length: 300mm - Grain Diameter: 57mm ### Area Graph ![](https://hackmd.io/_uploads/HJ0-1EvR3.png) ### Manufacturing Process ## Reference - MIL-HDBK-5H: https://ssrl-uark.com/MILHDBK5H.pdf - Rocket motor classification: https://en.wikipedia.org/wiki/Model_rocket_motor_classification - O-Ring Spec: https://www.yuenchin.com/uploads/catalog/5ebea0601e9d2fe060ced486833820b0.pdf - ISO 898-1: http://fpg-co.com/Standards/ISO898-1.pdf