SPACEX · VEHICLE PROFILE · DATA AS OF 2026-05-14
Falcon 9 (all variants)
Operational
First-stage reusable
Medium
528
Flights
Success / Partial / Failure
99.43%
Success Rate
525/528 flights
34×
Fleet Leader
B1067
May 12, 2026
Cadence
Last completed flight
RELIABILITY & S/PF/F SPLIT
99.43%
Overall success rate · Wilson 95% LB 98.34%
525
Success
1
Partial Failure
2
Failure
0
Scrubbed
Days since last failure671 days
Current success streak201
Last completed flightMay 12, 2026
Methodology IP
S/PF/F split is non-negotiable methodology. Partial failures are NOT collapsed into failures. A partial (e.g. payload delivered to wrong orbit, booster lost on otherwise-successful flight) is treated as a distinct outcome for underwriting. See /methodology/.
REUSE CURVE
Success rate by booster flight number — how this vehicle's flight-proven stages perform across reuses. Lower Wilson bound included for low-N flight counts.
| Flight | N | S / PF / F | Breakdown | Success | Wilson LB |
|---|---|---|---|---|---|
| Flight 1 | 76 | 74 / 1 / 1 | 97.4% | 90.9% | |
| Flight 2 | 46 | 46 / 0 / 0 | 100.0% | 92.3% | |
| Flight 3 | 35 | 35 / 0 / 0 | 100.0% | 90.1% | |
| Flight 4 | 24 | 24 / 0 / 0 | 100.0% | 86.2% | |
| Flight 5 | 25 | 25 / 0 / 0 | 100.0% | 86.7% | |
| Flight 6 | 20 | 20 / 0 / 0 | 100.0% | 83.9% | |
| Flight 7 | 21 | 21 / 0 / 0 | 100.0% | 84.5% | |
| Flight 8 | 17 | 17 / 0 / 0 | 100.0% | 81.6% | |
| Flight 9 | 22 | 22 / 0 / 0 | 100.0% | 85.1% | |
| Flight 10 | 19 | 19 / 0 / 0 | 100.0% | 83.2% | |
| Flight 11 | 19 | 19 / 0 / 0 | 100.0% | 83.2% | |
| Flight 12 | 17 | 17 / 0 / 0 | 100.0% | 81.6% | |
| Flight 13 | 16 | 16 / 0 / 0 | 100.0% | 80.6% | |
| Flight 14 | 14 | 14 / 0 / 0 | 100.0% | 78.5% | |
| Flight 15 | 14 | 14 / 0 / 0 | 100.0% | 78.5% | |
| Flight 16 | 16 | 16 / 0 / 0 | 100.0% | 80.6% | |
| Flight 17 | 12 | 12 / 0 / 0 | 100.0% | 75.7% | |
| Flight 18 | 10 | 10 / 0 / 0 | 100.0% | 72.2% | |
| Flight 19 | 10 | 9 / 0 / 1 | 90.0% | 59.6% | |
| Flight 20 | 9 | 9 / 0 / 0 | 100.0% | 70.1% | |
| Flight 21 | 11 | 11 / 0 / 0 | 100.0% | 74.1% | |
| Flight 22 | 6 | 6 / 0 / 0 | 100.0% | 61.0% | |
| Flight 23 | 7 | 7 / 0 / 0 | 100.0% | 64.6% | |
| Flight 24 | 5 | 5 / 0 / 0 | 100.0% | 56.6% | |
| Flight 25 | 4 | 4 / 0 / 0 | 100.0% | 51.0% | |
| Flight 26 | 4 | 4 / 0 / 0 | 100.0% | 51.0% | |
| Flight 27 | 4 | 4 / 0 / 0 | 100.0% | 51.0% | |
| Flight 28 | 2 | 2 / 0 / 0 | 100.0% | 34.2% | |
| Flight 29 | 3 | 3 / 0 / 0 | 100.0% | 43.8% | |
| Flight 30 | 3 | 3 / 0 / 0 | 100.0% | 43.8% | |
| Flight 31 | 2 | 2 / 0 / 0 | 100.0% | 34.2% | |
| Flight 32 | 2 | 2 / 0 / 0 | 100.0% | 34.2% | |
| Flight 33 | 2 | 2 / 0 / 0 | 100.0% | 34.2% | |
| Flight 34 | 1 | 1 / 0 / 0 | 100.0% | 20.7% |
Fleet Leader
B1067 · 34 flights. Registry: B1067 flight 26+.
Low-N caveat: 14 reuse bucket(s) have fewer than 10 flights. Point estimates should be read alongside the Wilson lower bound.
RECENT FLIGHTS
| Date | Mission | Payload | Outcome | |
|---|---|---|---|---|
| May 12, 2026 | NROL-172 | — · 22,800 kg | Success | |
| May 06, 2026 | Starlink Group 17-29 | LEO · 22,800 kg | Success | |
| May 03, 2026 | CAS500-2 & Others | SSO · 22,800 kg | Success | |
| May 01, 2026 | Starlink Group 10-38 | LEO · 22,800 kg | Success | |
| Apr 30, 2026 | Starlink Group 17-36 | LEO · 22,800 kg | Success | |
| Apr 26, 2026 | Starlink Group 17-16 | LEO · 22,800 kg | Success | |
| Apr 23, 2026 | GPS III SV10 | LEO · 22,800 kg | Success | |
| Apr 21, 2026 | GPS III SV10 | MEO · 22,800 kg | Success | |
| Apr 19, 2026 | Starlink Group 17-22 | LEO · 22,800 kg | Success | |
| Apr 15, 2026 | Starlink Group 17-27 | LEO · 22,800 kg | Success |
PAYLOAD & ORBIT MIX
12.0M kg
Total mass lifted
LEO
Most-flown orbit
0% gov
Gov / commercial split
0
Crewed flights
LEO16 (84.2%)
SSO2 (10.5%)
MEO1 (5.3%)
OPERATOR CONTEXT
OperatorSpaceX
Fleet success rate97.16%
Total fleet launches564
Vehicles operated7
REGISTRY DATA
First flight2018-05-11
Registry launches584 (as of 2025-12-31)
ClassMedium
Height70 m
Fairing diameter5.2 m
First-stage propellantkerolox
ReusabilityFirst-stage reusable
Recovery methodsRTLS, ASDS, expendable
First recovery success2015-12-21
Booster naming\bB1\d{3}(?:-\d{1,2})?\b
List price$67.0M
Payload capacity (kg)
LEO22,800 kg
GTO8,300 kg
LEO (reusable)17,400 kg
GTO (reusable)5,500 kg
Source: space_launch_vehicle_registry.json · Operator page →
METHODOLOGY
Per-vehicle reliability is aggregated from the AstraVeris launch_events table with Wilson 95% lower-bound error estimates. Subsystem outcomes are extracted by a local Gemma model from primary-source articles — outcomes are never fabricated; absence of a row means "not tracked". Aspirational vehicles (not yet flown) carry registry-only metadata with explicit "Not yet flown" banners. Full specifications: /methodology/. Licensing terms: /data-licensing/.
Not investment advice. For insurance underwriting, verify against operator investigation reports.