ORBITDECKMission Intelligence
Vehicles/Starship
DevelopmentSpaceXUnited StatesFirst Launch: 2023-04-20

Starship

Fully reusable super heavy-lift rocket designed for complete reusability, Moon bases, and Mars colonization.

Starship is a fully reusable, two-stage super heavy-lift launch vehicle currently under active development and orbital flight testing by SpaceX. Consisting of the Super Heavy first stage booster and the Starship spacecraft upper stage, it is the tallest, most powerful rocket ever flown in human history, generating over 16.7 million pounds of thrust from 33 methane-fueled full-flow staged combustion Raptor engines.

SpaceStats Reliability & Flight Record

TOTAL LAUNCHES
6
Orbital missions
SUCCESSFUL
4
2 failures
SUCCESS RATE
66.7%
LANDINGS
3
Reusable First Stage
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Full Starship & Super Heavy Stack
SpaceXFeatured Photography
Full Starship & Super Heavy Stack
SpaceX

Architecture Analysis & Development Story

Engineering Dossier

History & Development

Originally unveiled under early project names including MCT, BFR, and Starship, the vehicle was designed from inception to achieve 100% full reusability for both stages. Early suborbital atmospheric hops in Starbase, Texas demonstrated the signature 'belly-flop' aerodynamic descent and flip-to-vertical landing maneuvers. Integrated orbital flight tests began in 2023, rapidly advancing stage separation via hot-staging rings, controlled oceanic soft splashdowns, in-space propellant transfer demos, and launch tower 'chopstick' mechanical catch recoveries of the Super Heavy booster.

Operational Record & Mission Impact

Selected by NASA as the Human Landing System (HLS) for the Artemis III and Artemis IV missions to return humanity to the lunar surface. Starship integrated flight tests have successfully proven hot-staging, controlled Super Heavy tower catches, and orbital velocity insertion.

Key Engineering Innovations & Design Highlights

33 Raptor 3 engines on Super Heavy producing over 74 MN (16.7 million lbf) of thrust using subcooled liquid methane and liquid oxygen (Methalox).

Full-Flow Staged Combustion (FFSC) engine cycle, eliminating problematic dynamic shaft seals and achieving extreme combustion efficiency.

Stainless steel 304L/30X alloy airframe offering superior cryogenic ductility and high-temperature strength during atmospheric re-entry.

Mechazilla launch tower recovery system using giant robotic catch arms ('chopsticks') to catch both returning Super Heavy boosters and Starship upper stages mid-air without landing legs.

Technical & Propulsion Specifications

Operator: SpaceX

Vehicle Dimensions & Mass

Overall Height
121.3 m
Body Diameter
9 m
Gross Lift-off Mass
5,000 t
Stages Count
2
Fairing Diameter
9 m

Super Heavy Booster

Main Engines
33x Raptor 2 / Raptor 3
Propellant
Subcooled LOX / Liquid Methane (CH4)
SL Thrust
73,500 kN
Vacuum Isp
350s
Dry Mass
200 t
Recovery Mode
Catch_Tower

Starship Spacecraft / Upper Stage

Upper Engine
6x 3x Raptor Sea-Level + 3x Raptor Vacuum (RVac)
LEO Capacity
150 t
GTO Capacity
63 t
TLI (Lunar)
50 t
Cost per Launch
$100,000,000
LEO Price / kg
~$667 / kg

Launch Complexes & Spaceports Network

2 Active Launch Pads
Orbital Pad A / Pad B
Starbase Orbital Launch Complex
Boca Chica, Texas, USA
25.997°N, -97.157°E
Launch Complex 39A (LC-39A Starship Mount)
Kennedy Space Center
Florida, USA
28.608°N, -80.604°E

Milestone & Historic Missions

Key Flight Achievements
2023-04-20Partial Failure

Integrated Flight Test 1 (IFT-1)

Customer: SpaceX

First integrated flight test clearing the orbital launch pad and demonstrating stage clearance.

2024-10-13Success

Integrated Flight Test 5 (IFT-5)

Customer: SpaceX

Historic first mid-air mechanical catch of the Super Heavy booster returning to the launch tower chopsticks.

SpaceStats Launch Manifest & Database

1 mission records cataloged in database

Full Space Calendar
Flight / MissionOrbitLaunch DatePad / LocationBooster / LandingStatusDetails
Starship | Flight 14
Flight 14
N/ASep 30, 2026
Orbital Launch Pad 2
SpaceX Starbase, TX, USA
B1080
ASDS
TBDDetails →