SP9 Weekly Report 1 Page 1 of 9 Team # Date Massachusetts Institute of Technology Unified Engineering Spring 2004 16.030/16.040 System Problem 8 Report 1 Date: Group # Name 1 Name 2 Name 3 Name 4 Name 5 *You may use your own cover page. However, all the information on this cover page must be included on your cover page.SP9 Weekly Report 1 Page 2 of 9 Team # Date I. Build I.1 Build Goals I.1.1 System I.1.2 Wing I.1.3 Tail I.1.4 Payload Accommodation I.1.5 Propulsion I.1.6 Landing Gear I.1.7 (Subsystem) I.2 Build and Manufacturing Procedures I.2.1 System I.2.2 Wing I.2.3 Tail I.2.4 Payload Accommodation I.2.5 Propulsion I.2.6 Landing Gear I.2.7 (Subsystem) I.3 Build and Manufacturing Schedule I.3.1 System I.3.2 Wing I.3.3 Tail I.3.4 Payload Accommodation I.3.5 Propulsion I.3.6 Landing Gear I.3.7 (Subsystem) I.4 Build and Manufacturing Time Estimates and Actuals I.4.1 System I.4.2 Wing I.4.3 Tail I.4.4 Payload Accommodation I.4.5 Propulsion I.4.6 Landing Gear I.4.7 (Subsystem) Build and Manufacturing Time Estimates and Actuals Estimate [hrs] Actual [hrs] YTD Wing TailSP9 Weekly Report 1 Page 3 of 9 Team # Date Payload Accommodation Propulsion Landing Gear (Subsystem) Integration System Total I.5 Build Status, Problems, and Problem ResolutionI.5.1 SystemI.5.2 WingI.5.3 TailI.5.4 Payload AccommodationI.5.5 PropulsionI.5.6 Landing GearI.5.7 (Subsystem)SP9 Weekly Report 1 Team # Page 4 of 9 Date II. Test II.1 Test Goals II.1.1 System II.1.2 Wing II.1.3 Tail II.1.4 Payload Accommodation II.1.5 Propulsion II.1.6 Landing Gear II.1.7 (Subsystem) II.2 Test Procedures II.2.1 System II.2.2 Wing II.2.3 Tail II.2.4 Payload Accommodation II.2.5 Propulsion II.2.6 Landing Gear II.2.7 (Subsystem) II.3 Test Schedule II.3.1 System II.3.2 Wing II.3.3 Tail II.3.4 Payload Accommodation II.3.5 Propulsion II.3.6 Landing Gear II.3.7 (Subsystem) II.4 Test Time Estimates and Actuals II.4.1 System II.4.2 Wing II.4.3 Tail II.4.4 Payload Accommodation II.4.5 Propulsion II.4.6 Landing Gear II.4.7 (Subsystem) Test Time Estimates and Actuals Estimate [hrs] Actual [hrs] YTD WingSP9 Weekly Report 1 Page 5 of 9 Team # Date Tail Payload Accommodation Propulsion Landing Gear (Subsystem) Integration System Total II.5 Test Status, Problems, and Problem ResolutionII.5.1 SystemII.5.2 WingII.5.3 TailII.5.4 Payload AccommodationII.5.5 PropulsionII.5.6 Landing GearII.5.7 (Subsystem)SP9 Weekly Report 1 Page 6 of 9 Team # Date III. Training III.1 Training Goals III.1.1 System III.1.2 Ground Crew III.1.3 Pilot III.2 Training Procedures III.2.1 System III.2.2 Ground Crew III.2.3 Pilot III.3 Training Schedule III.2.1 System III.2.2 Ground Crew III.2.3 Pilot III.4 Training Time Estimates and Actuals III.2.1 System III.2.2 Ground Crew III.2.3 Pilot Training Time Estimates and Actuals Estimate [hrs] Actual [hrs] YTD Ground Crew Pilot Other System III.5 Training Status, Problems, and Problem ResolutionIII.5.1 SystemIII.5.2 Ground CrewIII.5.3 PilotSP9 Weekly Report 1 Page 7 of 9 Team # Date IV. System Performance IV.1 System Performance **PLEASE NOTE THE UNITS REQUESTED!** Fill in data that is available at the time that Report 1 is due System Performance Against Predicted Goals Design/Predict ed/ or Assumed Value Actual Value Ma - Mass of Aircraft [oz] b - Wing Span [in] c – Mean Aerodynamic Chord [in] Length [in] S – Wing Surface Area [in2] AR – Aspect Ratio W/S – Wing Loading (max weighted) [oz/ft2] Aileron Area [in2] Stabilizer Area [in2] Elevator Area [in2] Tail Area [in2] Rudder Area [in2] Wing Mass [oz] Aileron Mass [oz] Stabilizer Mass [oz] Elevator Mass [oz] Tail Mass [oz] Rudder Mass [oz] Landing Gear Mass [oz] Fuselage Mass [oz] Number of Servos Total Servo Mass [oz] Motor Controller Mass [oz] Receiver Mass [oz] Motor Mass [oz] Battery Mass [oz] Propeller Mass [oz] Motor Gear Mass [oz] Vc,weighted – Cruise Velocity (max weighted) [mph] Vc,empty – Cruise Velocity (empty) [mph] Re – Reynolds Number CL,cruise (max weighted) – Lift Coefficient CD,cruise (max weighted) – Drag CoefficientSP9 Weekly Report 1 Page 8 of 9 Team # Date D – Drag (weighted) [oz] P – Propeller Pitch [in] D – Propeller Diameter [in] P/D – Propeller Pitch-Diameter Ratio ηηηηprop - Propeller Efficiency Preq – Required Power (cruise, max weighted) [W] Not applicable Pm – Motor power (cruise, max weighted) [W] Not applicable RPM – Motor RPM (cruise, max weighted) Not applicable Im – Motor Current (cruise, max weighted) [A] ηηηηmotor – Motor efficiency (Pm/ Pin) Vs – Stall Speed (max weighted) [mph] CL,max (max weighted) – Lift Coefficient Not applicable Rmin – Minimum Turn Radius (max weighted) [ft] sg – Ground Roll (max weighted) [ft] T1 – Empty Lap Time [sec] T2 – Pit Crew and/or Repair Time [sec] L3 – Endurance Time [sec] Score [sec] IV.2 System Performance Problems, and Problem ResolutionSP9 Weekly Report 1 Page 9 of 9 Team # Date Appendix A. Build Log B. Test Log C. Training Log C.1 Ground Crew C.2 Pilot C.3
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