Home / Tracker / Vehicles / Falcon Heavy
SPACEX · VEHICLE PROFILE · DATA AS OF 2026-05-14

Falcon Heavy

Operational First-stage reusable Heavy
11
Flights
Success / Partial / Failure
100.00%
Success Rate
11/11 flights
1×
Fleet Leader
B1089
Oct 14, 2024
Cadence
Last completed flight

RELIABILITY & S/PF/F SPLIT

100.00%
Overall success rate · Wilson 95% LB 74.12%
11
Success
0
Partial Failure
0
Failure
0
Scrubbed
Days since last failureNo recorded failures
Current success streak11
Last completed flightOct 14, 2024
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 10 10 / 0 / 0
100.0% 72.2%
Fleet Leader
B1089 · 1 flights. Registry: B1052 flight 5+.

RECENT FLIGHTS

Date Mission Payload Outcome
Oct 14, 2024 Europa Clipper — · 63,800 kg Success
Jun 25, 2024 GOES U — · 63,800 kg Success
Dec 29, 2023 X-37B No. 2 F4 — · 63,800 kg Success
Oct 13, 2023 Psyche — · 63,800 kg Success
Jul 29, 2023 Echostar 24 — · 63,800 kg Success
May 01, 2023 Viasat-3.1 — · 63,800 kg Success
Jan 15, 2023 CBAS 2 — · 63,800 kg Success
Nov 01, 2022 LDPE-2 — · 63,800 kg Success
Jun 25, 2019 Prox-1 — · 63,800 kg Success
Apr 11, 2019 Arabsat 6A — · 63,800 kg Success

View all flights in the main tracker →

PAYLOAD & ORBIT MIX

701.8K kg
Total mass lifted
—
Most-flown orbit
0% gov
Gov / commercial split
0
Crewed flights

OPERATOR CONTEXT

OperatorSpaceX
Fleet success rate97.16%
Total fleet launches564
Vehicles operated7

Open operator financial profile →

REGISTRY DATA

First flight2018-02-06
Registry launches11 (as of 2025-12-31)
ClassHeavy
Height70 m
Fairing diameter5.2 m
First-stage propellantkerolox
ReusabilityFirst-stage reusable
Recovery methodsRTLS, ASDS, expendable
First recovery success2018-02-06
Booster naming\bB10[5-9]\d(?:-\d{1,2})?\b
List price$97.0M
Payload capacity (kg)
LEO63,800 kg
GTO26,700 kg
Mars16,800 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.