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    • Home (overview)
    • What is cislunar space
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    • Glossary · terms & definitions
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  • Cislunar glossary (terms & definitions)

    • Cislunar Space Glossary
    • Fundamentals

      • Absolute Range
      • Aerodynamic Coefficient
      • Aerodynamic Moment
      • Aerospace Vehicle
      • Allan Deviation (ADEV)
      • Ballistic Coefficient
      • Bi-Elliptic Transfer
      • Body Frame
      • Celestial Coordinate System
      • Celestial Sphere
      • Characteristic Velocity
      • Coverage Angle
      • Dual One-Way Ranging (DOWR)
      • Earth Ellipsoid
      • Earth Oblateness Perturbation
      • Earth-Centered Earth-Fixed Frame (ECEF)
      • Einstein Equivalence Principle (EEP)
      • Energy Parameter
      • Earth Observation (EO)
      • Finite Thrust Maneuver
      • Free-Flight Phase
      • Free-Flight Trajectory
      • Frozen Orbit
      • Gaussian Perturbation Equations
      • Geocentric Inertial Frame
      • GPS Time
      • Gravitational Potential
      • Gravitational Redshift
      • Gravity Turn
      • Gravity vs Gravitation
      • High Altitude Airship (HAA)
      • Hit Equation
      • Hohmann Transfer
      • Inertial Navigation System
      • Instantaneous Balance Assumption
      • In-Situ Resource Utilization (ISRU)
      • Julian Date
      • Kepler's Equation
      • Korea Multi-Purpose Satellite (KOMPSAT)
      • Lagrangian Perturbation Equations
      • Launch Azimuth
      • Launch Window
      • Lift-to-Drag Ratio
      • Load Factor
      • Longitudinal and Lateral Motion
      • Lunar Lander
      • Minimum Energy Trajectory
      • Near-space
      • Newton's Iteration Method
      • Nuri (KSLV-II)
      • Nutation
      • Optimal Velocity Inclination
      • Orbit Capture
      • Orbit Insertion Conditions
      • Orbital Elements
      • Orbital Equation
      • Orbital Maneuver
      • Orbital Phase
      • Orbital Transfer Vehicle
      • Passive Hydrogen Maser (PHM)
      • Perturbation Motion
      • Phasing Orbit
      • Pitch Program Angle
      • Powered Phase
      • Precession
      • Center of Pressure
      • Range Error Coefficient
      • Reentry Corridor
      • Reentry Phase
      • Repeat Ground Track Orbit
      • Reusable Launch Vehicle
      • Synthetic Aperture Radar (SAR)
      • Satellite Ring
      • Sequential Quadratic Programming
      • Skip Reentry
      • Solar Exposure Factor
      • Specific Angular Momentum
      • Specific Impulse
      • Stagnation Heat Flux
      • Standard Atmosphere
      • Stratospheric Airship
      • Subsatellite Track
      • Sun-Synchronous Orbit
      • Thrust-to-Weight Ratio
      • Thrust
      • Total Angle of Attack
      • Trajectory Equation
      • Trajectory Optimization
      • Trim Angle of Attack
      • True Anomaly
      • Tsiolkovsky Rocket Equation
      • Powered Phase Turning Process
      • Two-Body Problem
      • Coordinated Universal Time
      • Variation of Parameters
      • Velocity Frame
      • Velocity Inclination Angle
      • Vis-Viva Equation
      • Very Low Earth Orbit (VLEO)
      • Walker Constellation
      • Zero-Angle-of-Attack Reentry
    • Dynamics & math

      • A* Search Algorithm (A* Search)
      • A2PPO (Attention-Augmented Proximal Policy Optimization)
      • Action-Angle Variables
      • Backstepping Sliding Mode Control
      • Backward Stability Set
      • Bang-bang Control (Bang-bang Control)
      • Barycentric Synodic Coordinate System
      • Batch Deployment (Batch Deployment)
      • Bicircular Four-Body Problem
      • Birkhoff-Gustavson Normal Form
      • Buoyancy-weight Imbalance
      • Capture Set
      • Central Manifold
      • Chaos Effect
      • Clohessy-Wiltshire (CW) Equation
      • Co-state Normalization (Co-state Normalization)
      • Co-state Variables
      • Coasting Arc (Coasting Arc)
      • Continuation Method (Parameter Continuation)
      • Continuation
      • Cooperative Agent (CA)
      • CR3BP with Low-Thrust (CR3BP-LT)
      • Circular Restricted Three-Body Problem (CR3BP)
      • Curriculum Learning
      • Deep Deterministic Policy Gradient (DDPG)
      • Deep Reinforcement Learning
      • Detection Graph
      • Differential Correction
      • Differential Evolution (DE) Algorithm
      • Differential Games (Differential Games)
      • Direct Collocation
      • Dynamic Programming (Dynamic Programming)
      • Dynamic Target Method
      • Ephemeris Model
      • Equinoctial Orbital Elements (Equinoctial Orbital Elements)
      • Earth Restricted Three-Body Problem (ERTBP)
      • Fuel-optimal Control
      • Fuzzy Backstepping Control
      • Generalized Advantage Estimation (GAE)
      • Gaussian Process Regression
      • Geocentric Rotating Coordinate System (GRC)
      • Hamiltonian
      • Hybrid Cluster Particle Swarm Optimization (HCPSO)
      • Heteroclinic Orbit Transfer (Heteroclinic Orbit Transfer)
      • Hill Three-Body Problem
      • Homotopy Method (Homotopy Method)
      • Improved Baseline Control-Point Method (Improved Baseline Control-Point Method)
      • Impulsive Maneuver
      • Initial Value Optimization
      • Invariant Manifold (Invariant Manifold)
      • J2000 Geocentric Equatorial Coordinate System (J2000 Geocentric Equatorial Coordinate System)
      • Jacobi Constant (Jacobi Integral)
      • K-Means Clustering (K-Means Clustering)
      • K-Medoids Clustering (K-Medoids Clustering)
      • KD-Tree (KD-Tree)
      • Libration Point (Equilibrium Point)
      • Libration Point Spacecraft Body Coordinate System (Libration Point Spacecraft Body Coordinate System)
      • Libration Point Spacecraft Orbital Coordinate System (Libration Point Spacecraft Orbital Coordinate System)
      • Lindstedt-Poincare Method (Lindstedt-Poincare Method)
      • L2-centered Rotating Coordinate System (L2-centered Rotating Coordinate System, LRC)
      • LSTM Neural Network
      • Low-Thrust Transfer MDP Formulation
      • Mass Discontinuity (Mass Discontinuity)
      • Multi-Objective Monte Carlo Tree Search (MO-MCTS)
      • Modal Analysis
      • Monodromy Matrix
      • Monte Carlo Tree Search
      • Newton-Euler Equations
      • NSGA II (Non-dominated Sorting Genetic Algorithm II)
      • Pareto Optimality
      • Particle Swarm Optimization
      • Patch Point (Splicing Point)
      • Patched Method
      • Poincaré Map
      • Poincaré Section
      • Pontryagin's Maximum Principle
      • Pseudo-Arclength Continuation
      • Spacecraft Pursuit-Evasion Game
      • Q-Law Control Law
      • Quasi-Bicircular Problem (QBCP)
      • Quasi-Bicircular Four-Body Problem
      • Reachable Set
      • Reduced-Order Dynamic Equations
      • Regional Station-keeping Control
      • Regularization
      • Reinforcement Learning Enhanced Particle Swarm Optimization (RLEPSO)
      • Saddle-Point Strategy
      • Seven-node Model
      • Shooting Method
      • Six-DOF Motion Equations
      • Sliding Mode Control
      • Solar Radiation Pressure (SRP)
      • Stability Index
      • Stability Set
      • State-Dependent Traveling Salesman Problem (SDTSP)
      • State Transition Matrix (STM)
      • Static Lift
      • Strobe Map
      • Switching Function
      • Targeting Method
      • Thermo-mechanical Coupling Model
      • Thermodynamic Model
      • Two-Point Boundary Value Problem (TPBVP)
      • Trim Condition
      • Two-Dominant Invariant Manifold Method
      • Two-Level Differential Correction Method
      • Two-node Model
      • Variational Mode Decomposition
      • Zero-Effort Miss (ZEM)
      • Zero-Velocity Surface
    • Mission orbits

      • Apolune
      • Axial Orbit
      • Ballistic Capture Orbit
      • Butterfly Orbit
      • Cycler Trajectory
      • Distant Prograde Orbit (DPO)
      • DRO Constellation
      • Distant Retrograde Orbit (DRO)
      • Earth-Moon L1/L2 Halo Orbit (EML1/EML2 Halo)
      • Free-Return Trajectory
      • Full Lunar Surface Coverage Orbit
      • Halo Orbit
      • Heteroclinic Connection
      • Horseshoe Orbit
      • Hub-and-Spoke
      • Lissajous Orbit
      • Long Period Orbit
      • Low Prograde Orbit (LoPO)
      • Low-Energy Transfer Orbit
      • Low-Thrust Transfer Orbit
      • Lyapunov Orbit
      • Multi-Revolution Halo Orbit
      • Near-Rectilinear Halo Orbit (NRHO)
      • Orbit Identification
      • Orbit Keeping (Station-Keeping)
      • Parking Orbit
      • Perilune
      • Polynomial Constraint Station-Keeping
      • Primary Impulse Orbit Transfer
      • Prograde
      • Quasi-Periodic Orbit
      • Resonance Orbit
      • Retrograde
      • Short Period Orbit
      • Transfer Orbit
      • Triangular Libration Points
      • Vertical Orbit
    • Navigation & systems

      • Altitude Regulation
      • Autonomous Navigation
      • Cislunar Spatiotemporal Reference
      • Earth-Moon Hybrid Navigation
      • Extended Kalman Filter (EKF)
      • GPS Aided GEO Augmented Navigation (GAGAN)
      • Earth GNSS Weak Signal Navigation
      • Inter-Satellite Link Navigation
      • Indian Regional Navigation Satellite System (IRNSS)
      • LEO Navigation Augmentation
      • LiAISON Navigation
      • LunaNet (Lunar Network)
      • Lunar Navigation Constellation
      • Moonlight Initiative
      • Observability
      • Positioning, Navigation, and Timing (PNT)
      • Sun-Earth-Moon Autonomous Navigation
      • Tiandu-1
      • Trajectory Planning
      • X-ray Pulsar Navigation
    • Astronomy & observation

      • Astrometry
      • Background Star Elimination
      • Cislunar Moving Objects
      • Continuous Coverage (CP)
      • Earth Albedo
      • Ephemeris Correlation
      • Hot Pixel
      • Illumination Constraint
      • Image Registration
      • Image Stacking
      • Infrared Radiation
      • Lunar Glare Zone
      • Pointing Constraint
      • Quasi-zero Wind Layer
      • Segmentation Map
      • Shift-and-Add (SAA)
      • Sidereal Tracking
      • Signal-to-Noise Ratio (SNR)
      • Solar Radiation
      • Source Extraction
      • Synthetic Tracking
      • Zonal Wind
    • Military space doctrine

      • Anti-Satellite Test (ASAT)
      • Cislunar Space Situational Awareness
      • Civil-Military Integration
      • Competitive Endurance
      • Component Field Commands
      • Commander, Space Forces (COMSPACEFOR)
      • Counterspace Operations
      • Directed Energy Weapon (DEW)
      • Distributed Architecture
      • DOTMLPF-P Framework
      • Force Design
      • Force Development
      • Force Employment
      • Force Generation
      • Golden Dome
      • Kinetic Weapon
      • Mission Command
      • Mission Delta (MD)
      • Operational Test and Training Infrastructure (OTTI)
      • Persistent Detection Corridor (PDC)
      • Resilience Map
      • Resilient/Disaggregated Architecture
      • Space Domain Awareness (SDA)
      • Space Mission Task Force (SMTF)
      • Space Superiority
      • Space Force Generation Process (SPAFORGEN)
      • System Delta (SYD)
    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • Danuri Lunar Orbiter
      • General Dynamics Mission Systems
      • GITAI USA
      • Indian Space Research Organisation
      • Korea Aerospace Administration
      • Lockheed Martin
      • Northrop Grumman
      • Quindar
      • Raytheon Missiles & Defense
      • Sci-Tec
      • SpaceX
      • Satish Dhawan Space Centre SHAR
      • True Anomaly
      • Turion Space

SpaceX (Space Exploration Technologies)

Author: Tianjiang Shuo

Source: SpaceX Official Website and public sources

Site: https://cislunarspace.cn

Company Overview

SpaceX (Space Exploration Technologies Corporation) was founded by Elon Musk in 2002, headquartered in Hawthorne, California. SpaceX is a global leader in commercial space, with reusable launch vehicle technology as its core competitive advantage, having fundamentally transformed the cost structure of global launch services. SpaceX operates the world's largest constellation of orbiting satellites — Starlink — and is developing the fully reusable Starship launch system, which will be the largest launch vehicle ever built by humanity. SpaceX plays an irreplaceable role in cislunar space transportation, lunar missions, and deep space exploration.

Space and Cislunar-Related Business

Starlink Constellation

Starlink is SpaceX's low Earth orbit (LEO) internet constellation and the world's largest satellite constellation:

  • Scale: As of May 2025, the Starlink constellation has more than 8,460 satellites in orbit, with plans to eventually expand to approximately 12,000, and a final goal of 42,000 (FCC approved for 12,000).
  • Cislunar Space Communications: Starlink V2 Mini satellites are equipped with laser inter-satellite links (ISL), enabling data relay in cislunar space, and theoretically have the potential to extend to cislunar space communications support.
  • Earth Support: Starlink provides high-speed, low-latency internet services to ground users, demonstrating military communications support capabilities in the Russia-Ukraine conflict.

Falcon Launch Vehicle Family

SpaceX's Falcon rocket family is a main player in the current commercial launch market:

  • Falcon 9: A reusable two-stage launch vehicle with an LEO capacity of approximately 22.8 tons and GTO capacity of approximately 8.3 tons; the first stage booster can be reused multiple times. Falcon 9's frequent launches have given SpaceX a dominant share of the global launch market.
  • Falcon Heavy: Composed of three Falcon 9 first stages in parallel, with an LEO capacity of approximately 63.8 tons and GTO capacity of approximately 26.7 tons; it is one of the largest active launch vehicles in the world. Falcon Heavy has executed multiple national security and commercial missions.

Starship

Starship is SpaceX's next-generation fully reusable super-heavy launch system under development:

  • Scale and Capacity: Starship stands approximately 121 meters tall, with the first-stage "Super Heavy" booster equipped with 33 Raptor engines; the Starship upper stage can deliver 100-150 tons of payload to LEO, with a capacity of approximately 100 tons in fully reusable mode.
  • Lunar Missions: NASA has selected Starship as the Human Landing System (HLS) for the Artemis program, which will deliver astronauts from the Gateway (or directly) to the lunar surface in Artemis III and subsequent missions. In 2025, SpaceX designed a dedicated lunar Starship proposal for NASA's Artemis program, planning to use reusable Starship to improve lunar landing efficiency.
  • Cislunar Space Transportation: Starship's nearly 100-ton LEO capacity and on-orbit refueling capability make it a core transportation tool for future cislunar space infrastructure construction, capable of delivering large modules and supplies to cislunar L1 or NRHO.

Crew Dragon

SpaceX's Crew Dragon is the primary crewed spacecraft for NASA's Commercial Crew Program (CCP):

  • International Space Station Missions: Since 2020, Crew Dragon has executed multiple ISS crew transportation missions, delivering NASA astronauts to the International Space Station.
  • Cislunar Space Potential: Crew Dragon's design can be extended to support farther deep space missions, making it a candidate for future commercial cislunar travel.

Major Products and Technologies

Product/TechnologyTypeDescription
StarlinkSatellite Internet ConstellationLargest LEO broadband constellation, 8,460+ satellites in orbit
StarshipLaunch Vehicle/SpacecraftFully reusable, 100-ton LEO capacity, lunar lander
Falcon 9Launch VehicleReusable, 22.8-ton LEO capacity
Falcon HeavyLaunch VehicleThree boosters in parallel, 63.8-ton LEO capacity
Crew DragonCrewed SpacecraftCommercial crew, LEO missions
Raptor EngineLiquid Oxygen-Methane EngineStarship propulsion system, full-flow staged combustion cycle

Connection to Cislunar Space Missions

SpaceX is one of the most direct drivers of cislunar space economic development:

  • Revolution in Transportation Costs: Reusable Falcon 9 and the upcoming Starship have reduced cislunar space cargo transportation costs by more than an order of magnitude, making large-scale cislunar space infrastructure construction economically viable.
  • Core Artemis Contractor: As the HLS lunar lander supplier, SpaceX is a key element of NASA's crewed return-to-Moon program; Starship's maturity directly determines the Artemis implementation schedule.
  • Communications Infrastructure: Starlink constellation's laser inter-satellite link technology has validated the feasibility of space-based communications networks, which can be extended to become a cislunar space communications backbone.
  • On-Orbit Services Front: SpaceX is accumulating on-orbit satellite operations and maintenance experience through Starlink, which can be translated into engineering capabilities for on-orbit services.

Related Terms

  • Artemis Program: /en/research-frontiers/directions/security-governance/orbital-game/artemis/
  • Near-Rectilinear Halo Orbit: /en/glossary/orbits/nrho/
  • Distant Retrograde Orbit: /en/glossary/orbits/dro/

References

  • SpaceX Official Website: https://www.spacex.com
  • NASA Artemis, "SpaceX Starship HLS contract", 2021.
  • FCC, "Starlink Gen 2 approval order", 2022.
  • SpaceX Starship Launch Updates, 2024-2025.
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Last Updated: 6/5/26, 1:00 PM
Contributors: Hermes Agent, Ou Yang Jiahong
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