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Blue Origin — Landing Lidar System

FO Project: 158500 Last updated: 2026-04-07 (Session 93) — NG-3 imminent (Apr 10–14); Endurance TVAC at JSC ongoing; BE-7 hot-fire Q2 2026

Summary

Blue Origin flew one FO project (2024-2025) to mature a dual-mode landing lidar for lunar landing in variable lighting conditions — the most challenging part of polar lunar navigation, where permanent shadow craters make optical navigation fail. This project is almost certainly feeding into the Blue Moon MK1 uncrewed lunar lander, which is under development and targeting a 2026/2028 launch.

TRL note: The project is listed as "Completed" but TRL shows 4 (began 4, target 6 — did not reach target). This is unusual and suggests either (a) the project was completed as a feasibility/data collection milestone without formal TRL certification, or (b) TRL entry is not updated post-completion.

Important context: Blue Origin has a separate, earlier Tipping Point partnership with NASA (SPLICE, 2018–2021) that tested Navigation Doppler Lidar (NDL) from LaRC + Terrain Relative Navigation on New Shepard. The FO [158500] "Landing Lidar System" is a distinct, more recent project for Blue Origin's own proprietary lidar.

Chain: FO [158500] (2024–2025, dual-mode lidar feasibility) → Blue Moon MK1 landing system → MK1-SN001 "Endurance" pathfinder (late 2026) → VIPER delivery mission (late 2027)

FO Project Details

Project: 158500 — "Landing Lidar System"
Period: 2024-02-01 to 2025-12-31
TRL: 4 (began 4, target 6 — current: 4, did not advance)
TX: TX09.5 — Flight Mechanics and GN&C for Entry, Descent, and Safe Precise Landing
PI: Ryan Odegard (Blue Origin, LLC)
Lead Org: Blue Origin, LLC (Kent, WA)

What it was: NASA describes it as "Maturation of Robust Landing Lidar System" — a dual-mode lidar addressing variable lighting challenges on the lunar surface (continuously changing lighting, permanently shadowed polar regions where optical navigation fails). Targets low-mass, cost-effective, high-reliability design for commercial lunar missions.

What it achieved: TRL stayed at 4 — project completed as feasibility/data collection, not a flight demonstration. Likely the FO project funded early design and ground test, not a suborbital flight test (no flight vehicle mentioned).

Blue Origin's Lunar Landing Lidar Context

Earlier Program: SPLICE Tipping Point (2018–2021)

NASA's SPLICE (Safe and Precise Landing — Integrated Capabilities Evolution) used New Shepard as the test vehicle: - NDL (Navigation Doppler Lidar) from NASA LaRC (the same technology covered in psionic-ndl.md) - Terrain Relative Navigation software from Draper - Two New Shepard flights (NS-13 Oct 2020, NS-17 Aug 2021) - SPLICE Final Report: NTRS 20210026314

SPLICE tested NASA-developed tech aboard Blue Origin's vehicle. The FO [158500] is different: it's Blue Origin developing their own lidar.

Blue Moon MK1 Landing System

Blue Moon uses: - Flash lidar for terrain-relative navigation (autonomous safe zone selection) - Dual-mode lidar for variable lighting (polar missions to Shackleton Crater region) - Landing precision target: within 100m (first mission), single-digit meters (later flights) - SCALPSS payload ($6.1M): four cameras for plume-surface interaction data during descent

Blue Moon MK1 (cargo version, up to 3 metric tons to lunar surface) targets launch on New Glenn from LC-36, Cape Canaveral.

MK1-SN001 "Endurance" pathfinder (targeting late 2026): Vehicle left Blue Origin's production facility January 20, 2026 and was shipped to Houston. Named "Endurance" after Ernest Shackleton's ship that journeyed to Earth's South Pole — symbolizing operational resilience. February 2026: Transported to NASA Johnson Space Center for rigorous thermal vacuum testing in Chamber A (90-ft tall vacuum chamber, temp range -50°C to +30°C simulating lunar surface conditions). Full-duration BE-7 hot-fire integrated with flight tanks expected Q2 2026 in Huntsville, AL. Vehicle masses 21,350 kg, 8m tall (larger than Apollo LM), carries ~3,000 kg to lunar surface. Launch on New Glenn from LC-36. Target: lunar south pole near Shackleton Crater, landing precision within 100m.

VIPER delivery (late 2027): NASA formalized CS-7 task order to Blue Origin under CLPS in December 2025, total potential value $190M. Two-phased: (1) base design phase, then (2) option for actual landing — exercisable only after Endurance pathfinder succeeds. VIPER will conduct 100-day surface mission, 12-mile traverse, 3 day/night cycles. TRIDENT drill (Honeybee Robotics) samples volatiles to 1m depth.

New Glenn — Now Operational

New Glenn is proven and no longer a developmental risk for Blue Moon: - NG-1 (Jan 16, 2025): Reached orbit on maiden flight; first stage lost on descent - NG-2 (Nov 13, 2025): Launched NASA ESCAPADE; first stage successfully landed on drone ship "Jacklyn" — full reusability demonstrated - NG-3 (NET April 10–14, 2026): Imminent. AST SpaceMobile BlueBird Block 2 satellite (2,400 sq ft phased array, largest commercial comms array in LEO). First booster reuse — NG-2 first stage "Never Tell Me The Odds" flying again. First of multi-launch agreement for 45–60 BlueBird satellites. Launch from LC-36, Cape Canaveral. - New Glenn 9x4: Super-heavy-lift variant in development

Attribution Assessment

Is FO [158500] feeding into Blue Moon?
Confidence: suggestive.

Evidence for: (1) timing (FO project 2024–2025, Blue Moon in active development), (2) matching technology (dual-mode lidar, variable lighting, polar lunar missions), (3) Blue Origin is the prime, so internal technology flows naturally, (4) Blue Moon's published landing system includes exactly this type of lidar.

Evidence against: (1) TRL didn't advance (4→4), suggesting limited progress, (2) no explicit TechPort linkage, (3) Blue Origin may be using entirely separate internal resources for Blue Moon.

The most likely interpretation: FO funded a specific design study/ground test for a polar-capable landing lidar. Even without formal TRL advance, the data and design work informs Blue Moon's landing sensor architecture.

Blue Origin Portfolio Note

Blue Origin also has a Honeybee Robotics connection: Blue Origin acquired Honeybee Robotics in 2021. Honeybee has a separate FO project [145004] (POCCET dust removal tool, 2022–2025, TRL5→5 — also didn't advance). So Blue Origin subsidiaries have two FO projects in the recent cohort.

Honeybee recent wins (2025-2026): - Mars Sample Return SEM (Jul 2025): NASA awarded Honeybee the Spin Eject Mechanism contract for the Earth Entry System capsule release on MSR ERO. - IM-5 Lunar Rover (Mar 2026): Honeybee next-gen lunar rover hosting NIRVSS instrument suite on Intuitive Machines IM-5 ($180.4M CLPS mission). Notable: Honeybee hardware flying on a competitor's lander, not Blue Origin's MK1. - TRIDENT drill on VIPER: Confirmed as the onboard sampling instrument for VIPER on MK1 (2027).

Outcome Category

  • Active Pre-Market — MK1 Endurance pathfinder targeting late 2026; VIPER delivery targeting late 2027
  • Mission Infusion (expected) — FO lidar work feeding into Blue Moon polar landing system
  • New Glenn operational — launch vehicle risk retired after NG-1/NG-2 (2025)

Cross-References

  • psionic-ndl.md — NASA's NDL tested on New Shepard via SPLICE Tipping Point; different from this project but related program context
  • VIPER/Blue Origin: NASA reassigned VIPER to Blue Moon after Astrobotic Griffin issues (see astrobotic.md)

Investigated: Session 5 (2026-04-06). Updated Session 93 (2026-04-07). Sources: TechPort [158500]; Spaceflight Now (Oct 2025); SatNews (Jan/Dec 2025); Blue Origin press (Jan 20 & Feb 2026); Orbital Today (Feb 2026); Payload Space; NASASpaceFlight.com (Mar 2026); NextBigFuture (Apr 2026).