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The Satellite Cookbook
  • The Satellite Cookbook: Or How To Build A Satellite
  • Index
  • 🔧Part I: Space Mission Engineering
    • Introduction
      • What is Space Mission Engineering?
      • History
      • Technology, Applications, Economics
      • Key Players
    • Concurrent Engineering
      • Process
      • Objectives, Constraints, Requirements
      • Concept Definition
      • Mission Analysis & Utility
      • Formal Requirements
    • Space Environment
      • Space Environment and Space Weather
      • Earth's Magnetic Field
      • Radiation Belts
      • Microgravity
      • Orbital Debris
    • Astrodynamics & Mission Analysis
      • Space Geometry
        • Applications
        • Parameter Computation
        • Relative Motion
      • Orbits & Astrodynamics
        • Keplerian Orbits
        • Orbits of the Moon and Planets
        • Terminology
        • Orbit Perturbations, Geopotential Models, and Satellite Decay
        • Specialised Orbits
        • Orbit Maneuvers
        • Summary: Rules of Practical Astrodynamics
      • Orbit Design
        • Orbit Selection and Design Process
        • Orbit Performance
        • Orbit Cost
        • Selecting Earth-Referenced Orbits
        • Selecting Transfer, Parking, and Space-Referenced Orbits
        • Constellation Design
        • Interplanetary Orbits
    • Cost Estimating
      • Introduction to Cost Estimating
      • Estimating Tools
        • Botto-up Cost Estimator
        • Parametric Cost Estimators
        • Experience Based Cost Estimators
    • Financing & Law
      • Sources
        • Africa
        • Asia
        • Europe
        • North America
        • Oceania
        • South America
      • GAAP, Amortization and Return on Investment (ROI)
      • Law and Policy Considerations
  • 🛰️Part II: Spacecraft & Payload Design
    • Overview of Spacecraft Design
      • Spacecraft Design Process
      • Space System Design Drivers
      • Spacecraft Configuration Alternatives
      • Partitioning Spacecraft into Subsystems
      • Preliminary Spacecraft Budgets
        • Spacecraft Budget Tools
      • Design Evolution
      • Future of Spacecraft Design
    • Payload
      • Overview of Payload Design
        • Types of Space Payloads
        • Tradeoffs
        • Payload Design
        • Electromagnetic Spectrum
      • Communication Payloads
        • Space Mission Communications Architecture
        • Link Analysis
        • Payload Design
      • Observation Payloads
        • Payload Design
        • Payload Sizing
        • Evolution
    • Propulsion
      • Basic Rocket Equations
      • Staging
      • Chemical Propulsion Systems
      • Plume Considerations
      • System Design Elements
      • Electric Propulsion
      • Alternative Propulsion Systems
    • Subsystems
      • Control Systems
        • Attitude Determination and Control
        • Trajectory Navigation and Control
      • On Board Data Handling
        • Computer System Baseline
        • Preliminary Design
      • Communications
        • Power
        • Telemetry, Tracking, and Command (TT&C)
      • Power
      • Structure & Configuration
      • Thermal
    • Logistics and Manufacturing
    • Risk
    • Alternative Designs
  • 🚀Part III: Launch & Operations
    • Launch Vehicles
      • Vehicle Selection
      • History
      • Basic Mechanics of Launch
      • Launch Environments
      • Available Vehicles
    • Launch Operations
      • Launch Sites and Launch Restrictions
      • Launch Site Preparation
      • Readiness Reviews
      • Launch Site Access
      • Launch Site Training
      • Transporting the Spacecraft to the Launch Site
      • Launch Site Processing
      • Launch Day
      • Post Launch and Early Operations
      • Modernising Launch Operations
      • Common Mistakes
    • Ground System
      • Antenna Services
      • Data Accounting and Distribution Services
      • Ground System Driving Requirements and Sizing
      • Technology Trends
    • Mission Operations
      • Mission Planning and Operations Development
      • Mission Execution
      • Mission Termination and Post-Mission Activities
      • Best Practices
      • Future of Mission Operations
    • End of Mission
      • IADC End of Mission Guidelines
      • LEO Disposal Options
      • Non-LEO Disposal Options
      • Passivation
      • Disposal Planning
  • Ethics & Philosophy
    • Space exploration
    • Vanity projects
    • Is it worth it?
  • Additional reference material
    • ESA and ECSS documents
    • Satellite orbit and range parameters
    • Example mass and power budgets
    • Satellite Missions Catalogue
  • Build Your Own
  • Databases
    • CEOS ESA Database - Catalogue of Satellite Missions
  • Case study's
    • Radar Constellation
    • On-Orbit Servicing and Debris Removal
    • Mars
    • Starlink
  • Contact
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On this page
  • A Comprehensive Guide to Spacecraft System Design Drivers
  • Definition of a Spacecraft System Design Driver
  • List of all Spacecraft System Design Drivers
  • How to Use Spacecraft System Design Drivers
  1. Part II: Spacecraft & Payload Design
  2. Overview of Spacecraft Design

Space System Design Drivers

A Comprehensive Guide to Spacecraft System Design Drivers

The purpose of this guide is to provide a comprehensive overview of spacecraft system design drivers and explain what they are and how they can be used to improve the performance of spacecraft.

This guide is for spacecraft systems design engineers who are looking for ways to improve their designs.

Definition of a Spacecraft System Design Driver

A spacecraft system design driver is a factor that affects the performance of a spacecraft's systems. Design drivers can include everything from system components to environmental conditions.

List of all Spacecraft System Design Drivers

  • System requirements

  • Power system

  • Weight and balance

  • Thermal environment

  • Attitude control system

  • Propulsion system

  • Software and hardware design

  • Cost constraints

  • Environmental conditions

  • Launch vehicle requirements

How to Use Spacecraft System Design Drivers

There are several steps that should be followed when using design drivers to improve the performance of a spacecraft system:

Step 1: Identify System Requirements

The first step in designing a spacecraft system is to identify all of the requirements that the system must meet.

Step 2: Analyze the System

Next, analyze the system to determine how its components will interact with each other and the environment.

Step 3: Identify Design Drivers

Once the system is analyzed, identify all of the design drivers that could affect the performance of the system.

Step 4: Consider the Impact of Design Drivers on System Performance

Consider how each design driver will affect the performance of the system and determine which drivers will have the most significant impact.

Step 5: Create a Design Prototype

Create a prototype of the design to test its performance.

Step 6: Test the Prototype

Test the prototype to ensure that it meets all of the requirements.

Step 7:: Adapt and Improve the Design

Additional Resources

Here are some additional resources that you may find helpful:

  • Spacecraft System Design & Analysis: A Practical Approach - by J.P. Holman (ISBN: 978-0-89448-758-6)

  • Spacecraft Systems Engineering - by W.D. Cohen and G.L. Kulcinski (ISBN: 978-1-56347-566-0)

  • Introduction to Space Systems Design and Synthesis - by W.D. Cohen (ISBN: 978-0-88415-141-3)

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Last updated 2 years ago

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