
SpaceX — Starbase & Starship
Tracking the Starship program: Starbase infrastructure, flight cadence, rocket variants and Raptor industrialization.
AI-generated conceptual illustration — not experimental data.
How it worked
- Starbase (pads, towers, tanks, test stands)
- Super Heavy (Block 1/2 boosters)
- Starship V1/V2/V3 (vehicle architecture)
- Raptor 2/3 engines (sea level + vacuum)
- Ground chain: cryogenic GSE and turnover procedures

Purpose
Reach a reusable industrial loop (booster + ship), with orbital refueling and controlled return reliability.
Status, results & limitations
Current focus
- Shortening the gap between two flight campaigns
- Mastering return and recovery phases
- Validating engine configurations per mission variant
Risks / constraints
- Thermal complexity during reentry
- Regulatory windows and test cadence
- Dependence on the stability of the cryogenic supply chain
People & organisations
Roadmap & legacy
These dates and stages come from the earlier dossier. They are not a verified delivery schedule; listed objectives do not establish completed results.
- 2023-2024
Phase A — Integrated validation
Legacy reference — to verify- Combined booster + ship tests validated
- Starbase test architecture stabilized
- Abort and safety procedures strengthened
- 2025-2026
Phase B — Orbital cadence
Legacy reference — to verify- Ramp-up of ground preparation cadence
- Qualification of Starship V2/V3 variants
- Repeatable partial recovery of the stages
- 2027+
Phase C — Heavy operations
Legacy reference — to verify- Routine orbital refueling
- Multi-mission cadence per month
- Full industrialization of the maintenance cycle
Resources & evidence
Starbase progress
State of critical infrastructure and turnover capacity between two campaigns.
- Pad/tower availability per launch window
- Purge, fill and post-test safing capacity
- Average time to restore mission configuration
Rocket types and variants
Technical comparison of booster/ship variants by mission profile.
- Booster versioning (structure + engines)
- Starship V1/V2/V3 differences (mass, thermal, payload)
- Sea-level/vacuum engine configs per flight objectives
System reliability
Measuring robustness of the ground chain + vehicle over complete sequences.
- Rate of nominal sequences per campaign
- Analysis of rollback/abort causes
- Stability of post-flight procedures
Sources
Primary references for the organisations and technologies shown. They do not, by themselves, validate every claim or date in the inherited dossier.