Skip to content

Northrop Grumman — SSEP / NGHT-1X

Division: Tactical Space Systems (formerly Space Systems) | HQ: Baltimore, MD SST partnership: Annex to Collaborative Opportunity (ACO) with NASA Glenn Research Center Product: NGHT-1X Hall-effect thruster → Mission Extension Pod (MEP) satellite servicing

Last updated: 2026-04-14 (session 34)


SST Connection

SST Project Technology TRL Period Mechanism
116400 — Small Spacecraft Electric Propulsion (SSEP) NASA-H71M Hall thruster 4→5 2021-01 → 2024-09 ACO (Annex to Collaborative Opportunity)

PI: Eric J. Pencil (NASA GRC Project Manager) States: OH (GRC), VA (NG)

Unlike most SST projects where NASA funds a company, SSEP was a co-development: NASA GRC designed the H71M thruster; Northrop Grumman partnered via ACO to raise TRL through combined testing. NG then licensed the NASA technology for commercial use.


The Technology: NASA-H71M → NGHT-1X

The NASA-H71M is a sub-kilowatt Hall-effect thruster designed for small spacecraft with large delta-V needs:

Parameter Value
Input power 200–1,000 W
Specific impulse 1,750 s nominal (peak ~1,900 s)
Total impulse >2.5 MN-s (with 50% margin)
Propellant throughput >140 kg xenon
Delta-V capability >7 km/s for 180 kg spacecraft with 60 kg Xe

This is ~5× the total impulse of current state-of-the-art sub-kW Hall thrusters. A spacecraft using SSEP technology could self-propel from LEO to the Moon, or from GTO to Mars.

Northrop Grumman licensed the H71M as the NGHT-1X — their commercially available sub-kW Hall thruster. The technology flows from NASA to NG through formal IP licensing, not through a startup intermediary or acquisition.


Commercial Application: Mission Extension Pod (MEP) + Mission Robotic Vehicle (MRV)

SpaceLogistics, a wholly owned subsidiary of Northrop Grumman, developed the Mission Extension Pod (MEP) — a compact propulsion "jet pack" equipped with NGHT-1X thrusters, and the Mission Robotic Vehicle (MRV) — a robot-armed servicer that installs MEPs onto client satellites in GEO.

Architecture (updated session 34): 1. MRV launches to GEO carrying multiple MEPs 2. MRV uses robotic arms to install a MEP onto each client satellite 3. Each MEP extends host satellite life by 6+ years via NGHT-1X orbit-keeping 4. Host satellite operator avoids $200M+ replacement cost per satellite

Customers (3 confirmed): - Intelsat — 2 satellites serviced via MEP (ordered Apr 2023, service beginning 2026) - Optus — 1 satellite - All serviced by a single MRV hosting the MEPs

Timeline: - MRV with first 3 MEPs: eyeing 2026 launch (SpaceNews, Feb 2026). MRV is a next-generation platform beyond MEV - Builds on SpaceLogistics' MEV heritage — MEV-1 docked to Intelsat-901 (2020), MEV-2 to Intelsat 10-02 (2021)

MEP is smaller and cheaper than MEV (which uses NG's full-size satellite bus). The NGHT-1X enables MEP's compact form factor — high Isp with enough total impulse for GEO station-keeping. The MRV+MEP system scales servicing from 1-at-a-time (MEV model) to a multi-customer platform. Confidence: confirmed (SpaceNews, NG press releases, Intelsat announcement).


Testing and Validation

Long Duration Wear Test (LDWT): - Conducted at NASA GRC Vacuum Facility 11 (VF-11) - Funded by Northrop Grumman through fully reimbursable Space Act Agreement - Demonstrates full lifetime operational capability of NGHT-1X - Engineering Model development complete; progressing to qualification and flight unit build/test

NTRS publications (2 confirmed): 1. 20220007774 — "Overview and Performance Characterization of Northrop Grumman's 1 kW Hall Thruster String" (IEPC-2022-303, GRC, 2022). Authors: Nikrant, Glogowski, Cochran, Moquin, Choi. 2. 20230016674 — "NGHT-1X Pole Cover Erosion Measurements on Xenon and Krypton" (IEPC-2024, GRC, 2024). Authors: Nikrant, Switzer, Glogowski, Benavides, Baird.

Both papers published at IEPC (International Electric Propulsion Conference), the premier venue for EP technology.


Upstream Lineage

Source Period Connection
NASA GRC Hall thruster expertise Decades GRC is the institutional home for NASA Hall thruster R&D
NG MEV-1/MEV-2 satellite servicing 2020-2021 Proved the satellite life extension business model
SpaceLogistics subsidiary 2018+ Commercial entity for on-orbit servicing
SST ACO [116400] 2021-2024 Co-developed H71M; NG licensed as NGHT-1X

Downstream Impact

Outcome Details Confidence
NGHT-1X commercial thruster Licensed from NASA H71M, available for NG and potentially other platforms confirmed
MEP satellite servicing First 3 units launching 2025, each extending GEO comsat life 6+ years confirmed
New commercial market Satellite servicing is a multi-billion-dollar addressable market suggestive
NASA deep-space SmallSat enabler SSEP design enables LEO→Moon or GTO→Mars transit for 180 kg spacecraft suggestive
GRC wear test data Long-duration test at VF-11 generates public EP performance data confirmed

Assessment

Archetype: Defense Prime Technology Licensing — SST's only example of a defense prime co-developing with a NASA center and licensing the result for a commercial product. No startup risk, no acquisition needed.

What makes this distinctive: - Reverse flow: Most SST tech goes startup → acquisition by prime. Here, NASA center → prime directly. - Business model innovation: MEP is smaller/cheaper than MEV, enabled by NGHT-1X's compact high-performance. SST technology didn't just improve an existing product — it enabled a new product category. - Self-funding validation: NG pays for the wear test at GRC via reimbursable Space Act Agreement. The commercial customer is funding the government facility to validate the government's own technology — a mature public-private partnership. - Sub-kW sweet spot: NGHT-1X fills a performance gap — 5× better than existing sub-kW Hall thrusters. The SmallSat revolution needs exactly this: propulsion that lets small spacecraft do big maneuvers. - Only n=1 in SST: This is the only ACO-based technology licensing in the SST portfolio. Whether NASA can replicate this model with other primes is an open question.

Outcome: commercialized | Confidence: confirmed (ACO → license → product → 2025 launch manifest)