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BETA V600A

BETA V600A is an air-cooled direct-drive electric lift engine with four stators and four integrated inverters for vertical-flight applications. BETA publishes 314 kW continuous output and 470 kW maximum output, with 2,000 Nm continuous torque, 2,900 Nm maximum torque and a 1,500 rpm maximum shaft speed. Its 94.5 kg published weight is installed weight including the inverters.

Identity

Aliases
V600A
Domains
aviation
Identity Level
model
Kind
electric-motor
Name
BETA V600A
Status
active

Details

Description
BETA V600A is an air-cooled direct-drive electric lift engine with four stators and four integrated inverters for vertical-flight applications. BETA publishes 314 kW continuous output and 470 kW maximum output, with 2,000 Nm continuous torque, 2,900 Nm maximum torque and a 1,500 rpm maximum shaft speed. Its 94.5 kg published weight is installed weight including the inverters.
Developers
Dry Mass
…
Electric Motor Specs
Continuous Power
…
Continuous Torque
…
Cooling Type
air
Drive Configuration
direct-drive
Inverter Integration
integrated
Max Rpm
1,500
Peak Power
…
Peak Torque
…
Length
…
Lineage
-
Manufacturers
Propellants
-

Links

Assets & Meta

Creation Time
July 29, 2026 at 23:27:12 UTC
Updated Time
October 29, 2026 at 13:15:43 UTC

Other

Diameter
…
Sources
  • Accessed Date
    2026-07-29
    Note
    Names one H500A cruise motor and four V600A lift motors for ALIA VTOL.
    Publisher
    BETA Technologies
    Title
    Aircraft
  • Accessed Date
    2026-07-29
    Note
    Supports BETA's exact electric-motor product boundary and V600A ratings, integrated inverters, direct drive, and air cooling.
    Publisher
    BETA Technologies
    Title
    Motor