MonoLith™ Hypersonic
Power System
Mission-Critical Backup Power for Advanced Hypersonic Propulsion
Mission SpecificationsPerformance Specifications
Hover over any specification to explore its performance envelope.
Total usable energy for mission-critical backup power
Nominal bus voltage for vehicle power architecture
Peak voltage under full charge conditions
Sustained discharge power output for backup operations
Peak pulse discharge for transient load demands
Gravimetric energy density including enclosure and cooling interface
Total amp-hour capacity at nominal discharge rate
Complete system mass including enclosure and thermal interface
Complete Spec Sheet
Full electrical and environmental specifications.
Program Context
What makes this program unique.
Previous Supplier Failed
Brought in after the original battery supplier could not meet program specifications, with the program already behind schedule, EBS delivered on time.
Kerosene-Cooled Integration
The pack integrates into the vehicle’s kerosene thermal management system, where the same fuel used for hypersonic propulsion cools the battery pack, requiring precise thermal interface engineering.
Mission Override Capability
The system includes a mission override feature allowing operation beyond normal protective limits when mission continuation requires it, a requirement unique to critical aerospace programs.
System Architecture
Designed for direct integration into a kerosene-cooled hypersonic vehicle.
External PDU
- Power distribution unit is external to the pack
- Defined interface for vehicle integration
- Clean separation of power routing and storage
Fuel-Cooled Thermal Architecture
- Thermal management integrated into vehicle kerosene circuit
- No separate cooling system required
- Precise thermal interface engineering for fuel-as-coolant
Mission Override
- System can be commanded beyond normal BMS protective limits
- Mission-critical continuation capability
- Aerospace-specific requirement engineered to specification
Program Outcome
The program was behind schedule before we were contacted. The previous supplier had failed to deliver. We built the first unit on an aggressive timeline, integrated it into a kerosene-cooled thermal architecture unlike anything in our prior work, and delivered on time. They ordered two more.
Why It Matters
Called In After Supplier Failure
When the original supplier couldn’t deliver, this program needed a responsive, technically capable replacement. We delivered on time on a compressed schedule.
Fuel-Cooled Battery Integration
The pack interfaces directly with the vehicle’s kerosene thermal circuit, requiring thermal engineering beyond standard liquid cooling, a capability no catalog supplier offers.
Mission Override to Aerospace Spec
The ability to command a battery system beyond its protective limits for mission continuation is a rare, program-specific requirement we engineered and delivered.
Working on an advanced propulsion or aerospace program?
We build mission-critical battery systems for programs where the previous supplier couldn’t deliver. Responsive, technically capable, on schedule.