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Optimized Future-Proof Battery Pack for Aviation

  • Proprietary Aviation Battery Technology

  • In-House Developed Battery Management System (BMS)

  • Carbon Fiber Casing for Vibration and Thermal Runaway Protection

  • Unique Di-Electric Immersion Cooling Technique

  • Electric Aviation Battery Systems Optimized for Long Life and High Energy

  • Designed to Meet Electric Aviation Standards and Certifications

Rehabilitation & Sports
  • Cell connection in module
    96s4p
  • Nominal Energy (kWh)*
    8.3
  • Energy Density (Wh/kg)*
    260-270
  • Volumetric energy density (Wh/L)
    462
  • Voltage (max.)
    403
  • Cell type
    Cylindrical
  • Maximum Charge
    60amps (3C)
  • Maximum Discharge
    80amps (4C)
  • Protective rating
    IP67
  • Cooling type
    Immersion (Direct)
  • Applicable Standards
    DO-311A, DO-160, ARP-7131
  • Dimensions (L x W x H) in mm (nominal)
    591 x 185 x 164
  • Cycle life (GA flight profile, >80% DoD)*
    2000 (80% nom capacity retention)
  • Dry Weight
    31 kg

*subject to change with cell advancement

Prevention
  • Cell connection in module
    24s4p
  • Nominal Energy (kWh)*
    2.0
  • Energy Density (Wh/kg)*
    230
  • Volumetric energy density (Wh/L)
    369
  • Voltage (max.)
    100
  • Cell type
    Cylindrical
  • Maximum Charge
    54amps (3C)
  • Maximum Discharge
    72amps (4C)
  • Protective rating
    IP67
  • Cooling type
    Immersion (Direct)
  • Applicable Standards
    DO-311A, DO-160, ARP-7131
  • Dimensions (L x W x H) in mm (nominal)
    185 x 185 x 164
  • Cycle life (GA flight profile, >80% DoD)*
    2000 (80% nom capacity retention)
  • Dry Weight
    8.6 kg

*subject to change with cell advancement

Prevention
Prevention

Aircraft grade Master Battery Management System

Our BMS is designed to DAL B standard, with the possibility of certification to DAL A. Each Master BMS communicates with and controls up to four battery packs —each composed of two modules and one pack monitor— through a fail-safe reversible daisy chain communication system. It also supports CAN, Ethernet, and RS485 communication protocols for integration with the EPCU or other aircraft systems. Finally, it incorporates a powerful microcontroller capable of collecting battery data and performing advanced calculations for SoC, SoH, SoF, and other parameters.

Weight

250-275

Size

112 x 72 x 33 (mm)

P/N

Top

Parts

3

Circuit Boards

2
Prevention

Aircraft Grade Battery Power Distribution unit

The unit is modular, capable of integrating as many battery pack monitors as necessary. It measures pack current and voltage for State of Charge calculations and provides both charge and pre-charge discharge control. The system is liquid-cooled, using the same cooling circuit as the battery modules. For a configuration of four layers, the unit has an approximate weight of 16 kg (TBC). The BPDU dimensions for the proposed configuration are 295 × 225 × 168 mm.