Proprietary
Precision Composite Rocket Labs — Canada

Stage. Separate. Deploy.

Electromagnetic separation systems engineered from first principles. Non-explosive. Electronically triggered. Reusable. Validated across the full flight envelope — from ground to altitude.

441N
Holding Force
<10ms
Release Time
0%
Pyrotechnic
3000ft
Deployment Alt.
Flight Simulation — EM Separation Event PCRL-SIM-001
4800ft
3600ft
2400ft
1200ft
0ft
AGL
Separation ARMED
Pyro Status NONE
EM Magnet ACTIVE
Altitude ---
Wing Deploy STANDBY
Recovery READY
Electromagnetic Separation Vertical Launch Systems Rocket-to-Aircraft Transition Non-Explosive Deployment Swarm Deployment Capability Wing Deployment Systems Carbon Composite Airframes Pneumatic Recovery Electromagnetic Separation Vertical Launch Systems Rocket-to-Aircraft Transition Non-Explosive Deployment Swarm Deployment Capability Wing Deployment Systems Carbon Composite Airframes Pneumatic Recovery
01
Core Capabilities
CAP-001
Electromagnetic
Separation

Triaxial electromagnet array. Electronically triggered release replacing all pyrotechnic separation mechanisms. Complete reusability. Zero explosive certification requirements.

441N Force · <10ms Release · D30H22mm Array
CAP-002
Staged Wing
Deployment

Physics-driven sled deployment with counter-rotating synchronized actuation. Complete wing extension in under one second post-separation. Sensor-verified staged sequence.

<1s Deploy · Dual EM Lock · Fail-safe Parachute
CAP-003
Rocket-to-Aircraft
Transition

Single signal controls both stage separation and full aircraft conversion. Retracted during boost phase. Full control authority immediately post-separation. Circumvents guidance restrictions by transitioning vehicle classification.

T+3.0s Transition · Electric Pusher · Controlled Recovery
CAP-004
Vertical Launch System
Multi-Vehicle Deployment

Tube-array platform for sequential or simultaneous deployment of multiple rocket-aircraft vehicles. Shared electromagnetic separation timing enables coordinated wing deployment across all vehicles. Independent mission profiles post-separation. Scalable from dual to multi-vehicle configurations.

Single Platform · Coordinated Deploy · Independent Control Post-Sep
<50lb
Vehicle Launch Weight
60min
Mission Duration
25mi²
Search Coverage / Mission
500–3000ft
Deployment Altitude AGL
Design Philosophy
The separation event is the mission.
The rest is ballistics.

PCRL builds separation technology — not rockets. The rocket is a validation platform. The physics are the product. Non-explosive separation creates operational environments previously inaccessible to conventional systems: transport-unrestricted, storage-safe, electronically reconfigurable in the field. From amateur platforms through to orbital-class applications.

02
Application Areas
Defense · Tactical
Tactical
Deployment
Systems

Soldier-portable tube-launched vehicle platforms. Multi-unit VLS configurations deployable from ground vehicles. Non-explosive means standard logistics, no hazmat classification, no restricted storage. Rapid field reset. Coordinated swarm capability from single operator position.

VLS Platform No Hazmat Swarm Deploy Reusable IDEaS Eligible
Emergency Response · SAR
Rapid
Search &
Rescue

Rocket-boosted aerial search platform. 1000+ ft altitude in under 30 seconds. Transitions to 60-minute electric search aircraft. Deployable from emergency vehicles. All-weather launch independent of conventional drone limitations. Thermal imaging, GPS beacon deployment, multi-target coordinate storage.

SAR NIF Eligible 25mi² Coverage All-Weather GPS Beacon Drop
Aerospace · Research
High-Altitude
Research
Platform

Reusable upper stage with controlled landing capability. Eliminates vehicle loss — every flight returns data and hardware. Suitable for atmospheric sensing, payload demonstration, and separation system validation. Operates under existing amateur rocketry regulatory frameworks.

Reusable Controlled Recovery SR&ED Eligible Orbital-Scalable
Space · Commercial
Separation
Technology
Licensing

Electromagnetic separation as a licensable module for small satellite deployment, commercial launch vehicle staging, and orbital separation events. The "Intel Inside" model for aerospace separation. Non-explosive advantage eliminates range safety constraints at professional scale.

IP Licensing Small Sat Deploy Range Safety Orbital Class
03
Entity

Built
in Canada.
For What's
Next.

Precision Composite Rocket Labs is a Canadian federal corporation developing the world's first fully electromagnetic rocket separation ecosystem. Complete vertical integration from composite mandrel through final machining. No outsourced critical systems.

Operating under existing amateur rocketry frameworks while competitors navigate orbital regulatory complexity. Non-explosive advantage creates unrestricted global shipping, military logistics compatibility, and civilian airspace access unavailable to pyrotechnic systems.

Company Datasheet PCRL-ENT-001
IncorporatedJune 9, 2025
Corp Number#1706064-5
JurisdictionCanada Federal
LocationHanover, Ontario
Explosive ContentZero
Shipping ClassStandard / No Hazmat
ManufacturingFully Integrated
IP StatusProprietary
Regulatory PathDual-Use
SR&ED EligibleYes — 35% Refundable
Development StatusActive