BLUE ORIGIN · VEHICLE PROFILE · DATA AS OF 2026-04-27
New Glenn
OperationalFirst-stage reusableHeavy
3
Flights
Success / Partial / Failure
66.67%
Success Rate
2/3 flights
1×
Fleet Leader
NG-3
Apr 19, 2026
Cadence
Last completed flight
RELIABILITY & S/PF/F SPLIT
66.67%
Overall success rate · Wilson 95% LB 20.77%
2
Success
1
Partial Failure
0
Failure
0
Scrubbed
Days since last failure7 days
Current success streak0
Last completed flightApr 19, 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.
Low-N caveat: 1 reuse bucket(s) have fewer than 10 flights. Point estimates should be read alongside the Wilson lower bound.
SUBSYSTEM RELIABILITY
Per-system success rates aggregated across all flights with recorded subsystem outcomes. Systems without a row are "not tracked for this vehicle yet" — we never fabricate success.
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.