Spacecraft Design and Sizing Dr Andrew Ketsdever MAE

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Spacecraft Design and Sizing Dr Andrew Ketsdever MAE 5595 Lesson 14

Spacecraft Design and Sizing Dr Andrew Ketsdever MAE 5595 Lesson 14

Spacecraft Design and Sizing Introduction • Big Picture: The Mission drives the Payload and

Spacecraft Design and Sizing Introduction • Big Picture: The Mission drives the Payload and the Orbit, which drives the Spacecraft Design

Spacecraft Design and Sizing Overview of Spacecraft Design & Sizing

Spacecraft Design and Sizing Overview of Spacecraft Design & Sizing

Spacecraft Design and Sizing Principal Requirements & Constraints for S/C Design

Spacecraft Design and Sizing Principal Requirements & Constraints for S/C Design

Spacecraft Design and Sizing Principal Requirements & Constraints for S/C Design

Spacecraft Design and Sizing Principal Requirements & Constraints for S/C Design

Spacecraft Design and Sizing Weight Budget

Spacecraft Design and Sizing Weight Budget

Spacecraft Design and Sizing Spacecraft Configuration Drivers

Spacecraft Design and Sizing Spacecraft Configuration Drivers

Spacecraft Design and Sizing • Can use historical data for next block of same

Spacecraft Design and Sizing • Can use historical data for next block of same S/C, or to generalize within a mission type

Spacecraft Design and Sizing Mass Distribution for Selected Satellites

Spacecraft Design and Sizing Mass Distribution for Selected Satellites

Spacecraft Design and Sizing

Spacecraft Design and Sizing

Spacecraft Design and Sizing Mass Distribution for Selected Satellites

Spacecraft Design and Sizing Mass Distribution for Selected Satellites

Spacecraft Design and Sizing Top-Down Sizing Example • Given: navigation mission with m. P/L

Spacecraft Design and Sizing Top-Down Sizing Example • Given: navigation mission with m. P/L = 50 kg • Find: subsystem masses and mdry

Spacecraft Design and Sizing Top-Down Sizing Example • Still need other masses to permit

Spacecraft Design and Sizing Top-Down Sizing Example • Still need other masses to permit eventual launch vehicle choice • mkick is apogee kick motor – if needed • madapter counts against booster performance #s • Need to include margin

Spacecraft Design and Sizing S/C Budgets • For top-down designs, allocate so much of

Spacecraft Design and Sizing S/C Budgets • For top-down designs, allocate so much of a quantity or capability to each subsystem • Types of budgets – – – – Mass Power Communication bandwidth Volume Reliability Pointing error Cost Schedule, etc

Spacecraft Design and Sizing Mass Budget • See previous navigation S/C example → Now

Spacecraft Design and Sizing Mass Budget • See previous navigation S/C example → Now add mass margin into calculation • Margin covers the uncertainty in our estimates – Typical range from 5% to 25% – Larger margin for new S/C, or earlier in design phase – Smaller margin for known S/C, or as design progresses

Spacecraft Design and Sizing Preparing a Power Budget

Spacecraft Design and Sizing Preparing a Power Budget

Spacecraft Design and Sizing Typical Power Consumption by Module or Subsystem

Spacecraft Design and Sizing Typical Power Consumption by Module or Subsystem

Spacecraft Design and Sizing Propellant Budget • List v’s • Use ideal rocket equation

Spacecraft Design and Sizing Propellant Budget • List v’s • Use ideal rocket equation to convert v to propellant mass

Spacecraft Design and Sizing Propellant Budget

Spacecraft Design and Sizing Propellant Budget

Spacecraft Design and Sizing Estimating Spacecraft Equipment Compartment Dimensions

Spacecraft Design and Sizing Estimating Spacecraft Equipment Compartment Dimensions