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LANDSPACE (BEIJING LANDSPACE TECHNOLOGY) · VEHICLE PROFILE · DATA AS OF 2026-05-14

Zhuque-2 / 2E

Operational Expendable Medium
3
Flights
Success / Partial / Failure
66.67%
Success Rate
2/3 flights
Fleet Leader
No booster telemetry
Dec 08, 2023
Cadence
Last completed flight

RELIABILITY & S/PF/F SPLIT

66.67%
Overall success rate · Wilson 95% LB 20.77%
2
Success
0
Partial Failure
1
Failure
0
Scrubbed
Days since last failure1247 days
Current success streak2
Last completed flightDec 08, 2023
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/.

RECENT FLIGHTS

Date Mission Payload Outcome
Dec 08, 2023 Tianyi-33 — · 6,000 kg Success
Jul 12, 2023 Dummy payload — · 6,000 kg Success
Dec 14, 2022 Zhixing 1B — · 6,000 kg Failure

View all flights in the main tracker →

PAYLOAD & ORBIT MIX

18.0K kg
Total mass lifted
Most-flown orbit
0% gov
Gov / commercial split
0
Crewed flights

OPERATOR CONTEXT

OperatorLandspace (Beijing Landspace Technology)

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REGISTRY DATA

First flight2022-12-14
Registry launches6 (as of 2025-12-31)
ClassMedium
Height49 m
Fairing diameter4.2 m
First-stage propellantmethalox
ReusabilityExpendable
List price$15.0M
Payload capacity (kg)
LEO6,000 kg
SSO4,000 kg

Source: space_launch_vehicle_registry.json

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.