Orbital Logistics
Move payloads and supporting hardware through mission phases with a system intended for repeat use, not one-time propulsion expenditure.
GLIDE
Transfer architecture for sustained orbital logistics.
GLIDE is a propellantless transfer system designed around high-level momentum exchange and tether-assisted operations. The public view focuses on mission utility and system logic, not protected implementation detail.
Primary Configuration
System Summary
GLIDE is built around three operating ideas.
Momentum Exchange
Use stored motion in the platform to support transfer events, allowing orbital energy to be managed as part of the architecture instead of solely through onboard propellant.
Tether-Based Systems
Apply tether-assisted mechanics at a high level to enable controlled interaction, transfer geometry, and operational flexibility across orbital tasks.
Transfer Logic
High-level concept, readable in sequence.
Prepare The Transfer State
The system manages its operating condition before a transfer event so the orbital interaction begins from a controlled baseline.
Exchange Momentum
During the transfer phase, GLIDE uses its architecture to shift momentum between the platform and mission element in a deliberate, bounded way.
Continue The Cycle
The objective is not a single maneuver. It is a repeatable logistics cycle that supports later transfers, staging, and orbital utility over time.
Planform View
Why Tether Assistance
Because orbital transport is a mass problem before it is a marketing problem.
Transfer propellant drives launch mass, vehicle sizing, and payload margin. A tether-assisted system changes that discussion by making momentum management part of the vehicle architecture.
Payload Margin
Less dependence on dedicated transfer propellant can preserve useful mass for the mission itself.
Repeatable Utility
The same logistics platform can support multiple transfer cycles when the mission architecture is designed around continuity.
Architecture Flexibility
Operators gain options for staging, hosted payload placement, and orbital support functions that are difficult to sustain with single-use approaches.
Program Fit
GLIDE is aligned with practical orbital use cases.
Payload Transfer
Support mission elements that need relocation or insertion support after launch.
Orbital Staging
Enable infrastructure concepts that depend on movement between operational nodes.
Hosted Systems
Create a path for integrated hardware packages that benefit from shared logistics support.
Long-Duration Utility
Position transfer as a persistent service layer rather than a single mission event.
Renders
Configuration views.
Engage