teleo-codex/entities/space-development/sr-1-freedom.md

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---
type: entity
entity_type: protocol
name: SR-1 Freedom
parent_org: NASA
domain: space-development
secondary_domains: [energy]
status: active
announced: 2026-03-24
launch_date: 2028-12
supports:
- Nuclear electric propulsion (NEP) provides higher efficiency for uncrewed cargo missions while nuclear thermal propulsion (NTP) remains superior for crewed time-constrained missions
- Repurposing sunk-cost hardware for new missions can accelerate technology deployment timelines by 5-10 years compared to clean-sheet programs
reweave_edges:
- Nuclear electric propulsion (NEP) provides higher efficiency for uncrewed cargo missions while nuclear thermal propulsion (NTP) remains superior for crewed time-constrained missions|supports|2026-04-17
- Repurposing sunk-cost hardware for new missions can accelerate technology deployment timelines by 5-10 years compared to clean-sheet programs|supports|2026-04-17
---
# SR-1 Freedom
**Type:** Nuclear Electric Propulsion (NEP) spacecraft
**Mission:** Mars transit demonstration
**Launch:** December 2028
**Status:** Active development
## Overview
SR-1 Freedom is NASA's first nuclear-powered interplanetary spacecraft, announced March 24, 2026 alongside Project Ignition. It repurposes Gateway's Power and Propulsion Element (PPE) as the propulsion system for a nuclear electric spacecraft.
## Technical Architecture
**Propulsion:** Nuclear Electric Propulsion (NEP)
- Ion thrusters powered by fission reactor
- Distinct from Nuclear Thermal Propulsion (NTP)
- Uses Gateway PPE (already built) as propulsion module
**Mission Profile:**
- Launch: December 2028
- Destination: Mars transit demonstration
- Objective: Validate NEP for deep-space operations
## Strategic Context
SR-1 Freedom represents NASA's pivot to nuclear propulsion for interplanetary missions. The repurposing of Gateway's PPE (following Gateway's cancellation) demonstrates adaptive reuse of existing hardware to accelerate nuclear propulsion development.
**NEP vs NTP distinction:** Nuclear Electric Propulsion (ion thrusters + reactor) provides high specific impulse but low thrust, suitable for cargo missions. This is architecturally different from Nuclear Thermal Propulsion (heated propellant) which provides higher thrust for crewed missions.
## Timeline
- **2026-03-24** — SR-1 Freedom announced; Gateway PPE repurposed as propulsion module
- **2028-12** — Scheduled launch to Mars
## Related Programs
- [[project-ignition]] — Lunar surface program announced simultaneously
- [[gateway]] — Cancelled program whose PPE module was repurposed
## Sources
- Singularity Hub: "NASA Unveils $20B Moon Base Plan and Nuclear Spacecraft for Mars" (March 27, 2026)
- NASA.gov: "NASA Unveils Initiatives to Achieve America's National Space Policy" (March 24, 2026)