Below are the FAQ we have been asked. If you query is not addressed, please send it to: ior-wg@inorbitrefueling.org
About IOR-WG
1. What is the objective of IOR-WG?
Enable multi-vendor interoperability for in-orbit refueling.
Allow independent vendors to build compatible components that operate together as an IOR ecosystem, rather than a single end-to-end solution.
2. Why IOR-WG – our belief
For IOR to be economically viable, multiple providers must deliver interoperable components that serve many satellites.
Similar to terrestrial fuel ecosystems, infrastructure and consumers must be decoupled but compatible.
3. What is the focus of IOR-WG?
• Exclusive focus on In-Orbit Refueling (IOR)
• Deep focus at the interface, implementation and verification
• Covers: mission → system → interfaces → verification
4. Who is behind IOR-WG?
A small group of systems engineers with space and aerospace experience.
Initial interest from industry participants (service providers, manufacturers, technology vendors).
5. Who should participate?
• Satellite manufacturers
• Service vehicle providers
• Depot providers
• Resupply providers
• Ground segment providers
• IOR Service Providers
• Resupply Service Providers
• Technology providers (RPOD, sensors, propulsion, comms)
6. What is the long-term vision?
An interoperable IOR ecosystem where:
• Components are built independently
• Interfaces are standardized
• Technologies (RPOD, sensors, propulsion, comms) integrate seamlessly
7. How does IOR-WG operate?
• Driven by use cases, mission needs, and interface gaps
• Iterative and industry feedback-driven
• Produces implementation-ready artifacts, not just concepts
8. How is IOR-WG different from CONFERS?
IOR-WG uses outputs from CONFERS and others to build implementation-ready frameworks.
• CONFERS: guidelines → standards → SDO pipeline
• IOR-WG: interface definition + compliance/IVV readiness (pre-standard stage)
9. Where does IOR-WG fit in the ecosystem?
Operates upstream of formal standardization.
Delivers implementation-ready documentation aligned with existing guidelines and standards from organizations such as CONFERS and relevant SDOs.
10. What does IOR-WG deliver?
Ready for implementation and verification documents:
• Interface Requirements Document (IRD)
• Interface Control Document (ICD)
• Verification & Validation Plan (V&V Plan)
• Requirements Traceability Matrix (RTM)
• Compliance Matrix
General: In-Orbit Refueling Work Group
Q1: What kind of details can you share about your new initiative?
A1: This IOR initiative is a systems engineering architecture study focused on in-orbit refueling (IOR). It structures the problem from mission context and operational scenarios through to system architecture.
The objective is to create a common framework that brings together ISAM/RPOD providers, satellite manufacturers, and constellation operators to enable a more standardized refueling ecosystem.
We have developed artifacts covering mission context, stakeholders, operational scenarios, and system boundaries. A short excerpt from the CONOPS section is attached for context.
We also support companies in aligning their systems with the IOR framework through systems engineering, embedded software development, and verification and certification support.
Q2: Have you looked at any existing studies, missions, vehicle architecture, etc to see how it integrates with your proposed framework?
A2: To develop a common framework, we are currently:
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Adapting and aligning with guidelines from standards such as CONFERS, IRSIS, and ESA
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Supporting SERB-approved physical interfaces (e.g., Northrop Grumman’s PRM and Orbit Fab’s RAFTI)
With the objective of creating a truly common IOR framework, we are defining standardized interfaces for:
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Inter-Spacecraft Interfaces
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Physical (Docking/Transfer) – These are the two SERB-approved physical interfaces.
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Proximity Operations and Relative Navigation – Defines how two spacecrafts interact across three supported capability levels: IOR Enabled, IOR Aware, and IOR Cooperative. Definitions are provided in Appendix: 1.11.0: Terminology and Definitions.
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Inter-Ground System Interfaces
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Service Provider <-> Client Operator Ground Systems– Defines how the service provider and client operator coordinates planning, authorization, and execution of services.
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Service Provider <-> Resupply Provider– Supports resupply providers to coordinate and deliver propellant to the service provider in a standardized manner.
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Ground Systems to Spacecraft Interfaces
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Service Provider Ground System <-> Service Vehicle – Supports command, mission planning, and execution of servicing operations.
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Client Operator Ground System <-> IOR Cooperative Client Spacecraft – Provides telemetry, health monitoring, and coordination support for servicing activities to IOR System
These interfaces are intended to enable companies to develop compliant components and participate in a shared IOR ecosystem.
Q3: Are you looking for inputs to this at a high level?
A3: Yes, we are currently seeking input on:
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Nominal and off-nominal CONOPS
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System requirements
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External interface definitions
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Physical architecture and key components
Q4: How does it work exactly? Do you have a team of volunteers working on this initiative and/or do you have companies affiliated with the initiative?
A4: We are a team of systems engineers and MBSE professionals with space/aerospace backgrounds who are contributing on a voluntary basis.
As of early April, we have received engagement interest from six organizations, including both startups and established space companies. These companies include spacecraft manufacturers and on-orbit service providers.
Q5: Satellite and its subsystems’ design are highly proprietary. How is that taken into account?
A5: The initiative provides guidelines for systems providers for implementation to comply with the IOR framework. The implementation work is performed by system owners to align their systems with these guidelines.
The initiative focuses on interoperability covering the following interfaces:
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Physical (Docking/Transfer) – These are the two SERB-approved physical interfaces.
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Proximity Operations and Relative Navigation – Defines how two spacecrafts interact across three supported capability levels: IOR Enabled, IOR Aware, and IOR Cooperative. Definitions are provided in Appendix: 1.11.0: Terminology and Definitions.
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Service Provider to Client Operator Ground Systems Interface – Defines how the service provider and client operator coordinate planning, authorization, and execution of services.
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Service Provider Ground Systems to Satellite Interface – Covers command, mission planning, and execution of refueling operations.
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Service Provider to Resupply Provider Interface – Enables resupply providers to coordinate and deliver propellant to the service provider in a standardized manner.
Q6: How is the IP managed? Is it shared IP?
A6: Each participating company develops, manages, and retains ownership of its own intellectual property.
This initiative focuses only on defining interfaces between components, ensuring that independently developed solutions can interoperate when they comply with the defined interface standards.
Companies can bring IP which complies with the IOR system and license IP to its customers. For example:
A company may develop a docking and propellant transfer interface device (e.g., a RAFTI-like interface) that is compliant with the IOR Initiative. The company retains ownership of the device design and may license or supply it directly to users.
A LiDAR vendor may provide LiDAR technology compliant with the IOR Initiative and license its implementation directly to customers.
Q7: How do you support participating companies. Do you provide services to support the efforts?
A7: Yes, we support participating companies in aligning their systems with the IOR framework.
This includes systems engineering, embedded software development, and verification and validation support to ensure their components integrate cleanly within the broader architecture.
Where required, we also support traceability and certification readiness so that solutions are not only compliant at the interface level but are also deliverable within real program constraints.
Q8: Why are you doing this initiative?
Multipronged reasons:
Primary:
To create an open structure where companies can collaborate and deliver their parts based on clear interfaces and specifications—so together we can enable a practical, end-to-end IOR system.
Secondary:
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Build a services layer to support companies that need help with systems engineering, MBSE, or integration
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Build a compliance layer so IOR components can actually be verified against defined standards—not just documented
Q9: What types of folks are involved?
Team, companies and organizations are evolving. This is current state:
Started with Sanjay Chadha, now a small core team of 5 covering systems engineering, MBSE, architecture, and support functions.
We also have early interest from 6 companies and 1 space-supporting organization, and that’s growing as conversations progress.
Q10: What’s your desired outcome?
An IOR system deployed in space, enabling refueling based on standards generated under this initiative.
We are experts in real-world issues, so we can assist companies as they launch their ISAM, RPOD, or space products or IOR services.
Q11: Have you considered working with larger organizations like CONFERS or AIAA?
We review and follow CONFERS and IRSIS, and build on top of efforts from these organizations.
Yes, we are bringing our efforts to CONFERS and IRSIS member companies through general outreach and engagement. We appreciate introductions.
Q12: Are you a Canadian company?
Yes, although ReliqAI is a Canadian company, the IOR initiative work is supported internationally.
We are not supported by any Canadian funding, and the work is not constrained geographically—we can move and expand this work across international boundaries.