CSIS ‘Last Rounds’: Half of Prewar Inventory Expended on Four US Munitions in Iran War

THAAD launcher emplaced and ready to fire interceptors in the CENTCOM area of responsibility
Photo: U.S. Army / DVIDS / Public Domain — A Terminal High Altitude Area Defense (THAAD) launcher emplaced and prepared to fire interceptors in the CENTCOM area of responsibility. The THAAD interceptor is a hit-to-kill system with no explosive warhead; the kill vehicle impacts at closing velocities exceeding 2 km/s. The appearance of U.S. Department of Defense visual information does not imply or constitute DoD endorsement.

Intelligence Summary

The Center for Strategic and International Studies (CSIS) has published “Last Rounds? Status of Key Munitions at the Iran War Ceasefire,” the first credible open-source quantification of US precision munition expenditure across the 39-day air-and-missile campaign. The assessment covers seven key munitions across two operational categories: long-range land-attack and air-and-missile defence (AMD) interceptors. CSIS concludes that the United States may have expended more than half of its prewar inventory on four of the seven systems. Replacement timelines across the portfolio range from one to four years, conditional on existing pipeline deliveries arriving on schedule — a caveat with significant industrial-base sensitivity.

Open-source reporting corroborates the CSIS depletion picture. US official statements cited expenditure of “more than 1,000” BGM-109 Tomahawk Land Attack Missiles (TLAMs) and “1,500 to 2,000” AMD interceptors during the 39-day campaign. At pre-campaign production rates, replacing 1,000 TLAMs alone would require approximately five to seven years of uninterrupted Raytheon output. The AMD figure, dominated by Patriot Advanced Capability-3 Missile Segment Enhancement (PAC-3 MSE) rounds, represents several years of Lockheed Martin’s Camden, Arkansas production capacity.

At pre-surge production rates, replacing 1,000 TLAMs requires approximately five to seven years of Raytheon output. The campaign consumed, in 39 days, what the industrial base cannot replace in this decade without structural investment.

Weapon System Technical Assessments

BGM-109 Tomahawk Land Attack Missile (TLAM) — Block IV / Block V

The BGM-109G/H Tomahawk is a subsonic, sea- and ground-launched cruise missile designed for long-range precision strike against fixed and relocatable targets. Block IV (Tactical Tomahawk) introduced a two-way data link enabling in-flight retargeting; Block V added the Maritime Strike Tomahawk (MST) anti-ship variant and enhanced penetrating warhead.

ParameterBlock IV / Block V Data
Overall length (with booster)5.56 m
Body diameter0.52 m
Launch weight~1,315 kg (with booster)
Warhead — Block IVWDU-36/B unitary penetrating; explosive fill PBXN-107 (approximately 170 kg net explosive quantity — NEQ), HD 1.1, CG D
Warhead — Block V penetratorEnhanced penetrating warhead; NEQ DATA GAP (not in open release)
Propulsion (sustainer)Williams International F415-WR-400/402 turbofan; ~3.1 kN thrust
Propulsion (booster)Atlantic Research solid-fuel rocket booster, jettisoned post-launch; HD 1.3 during transport
Range>1,600 km (Block IV); Block V range DATA GAP
Speed~880 km/h (Mach 0.72 subsonic)
GuidanceInertial navigation + TERCOM terrain-following + DSMAC-IIA terminal optical scene matching + GPS
Circular error probable (CEP)<3 m (DSMAC terminal, against known aimpoints)
ProducerRaytheon Missiles & Defense, Tucson, AZ
Pre-surge production rateEstimated 150–200 rounds per year (open-source estimate; classified figure)
Unit cost (FY25 baseline)~USD 2.5–2.7 million per round
Storage hazardHD 1.1 (warhead section); HD 1.3 (booster in transit); CG D
Launch platformsMk 41 Vertical Launch System (surface ships); submarine torpedo tube or VLS; ground-based TLAM (BGM-109G legacy — retired)
DATA GAP: Annual US TLAM stockpile figure is classified. Open estimates range from 3,000 to 4,500 rounds pre-campaign. If the lower bound is accurate, expenditure of 1,000+ rounds represents a prewar inventory depletion of ~22–33% — consistent with, but at the lower end of, the CSIS “more than half” finding for the four most-depleted systems.

Precision Strike Missile (PrSM) — Block I

PrSM is the US Army’s replacement for the MGM-140 Army Tactical Missile System (ATACMS). Unlike ATACMS, which dispensed Dual-Purpose Improved Conventional Munitions (DPICM) or carried a unitary warhead, PrSM Block I carries a unitary warhead and is sized to two rounds per M142 High Mobility Artillery Rocket System (HIMARS) pod or four per M270A2 Multiple Launch Rocket System (MLRS) launcher, significantly increasing platform magazine capacity. PrSM entered limited operational service in 2023.

ParameterPrSM Block I Data
Launch weight~400 kg (estimated; classified programme)
Warhead typeUnitary blast-fragmentation; NEQ DATA GAP (classified)
HD / CGHD 1.1, CG F (estimated based on unitary warhead class; not confirmed in open release)
PropulsionSingle-stage solid rocket motor (SRM)
Range — Block I499 km (MTCR Category I ceiling; Missile Technology Control Regime compliance)
Range — Block II (developmental)>1,000 km (hypersonic glide vehicle integration planned)
GuidanceGPS/INS; anti-jam GPS receiver
Launcher compatibilityM142 HIMARS (2 rounds per pod); M270A2 MLRS (4 rounds per launcher)
ProducerLockheed Martin Missiles and Fire Control, Dallas, TX
Pre-surge production rateInitial rate; ramp-up ongoing. Figures classified.
Unit costDATA GAP; ATACMS comparator was ~USD 1.5M; PrSM expected higher
DATA GAP: PrSM production quantities and stockpile levels are not in open release. As the newest system in the CSIS seven, PrSM prewar inventory is likely the smallest, making percentage depletion figures most sensitive here even at relatively modest expenditure volumes.

Patriot Advanced Capability-3 Missile Segment Enhancement (PAC-3 MSE)

PAC-3 MSE is a hit-to-kill AMD interceptor deployed within the Patriot weapon system. Unlike earlier Patriot variants (PAC-1 and PAC-2 GEM), PAC-3 MSE does not rely on proximity-burst fragmentation. It carries a small “lethality enhancer” — a collar of focused fragmentation — but the primary kill mechanism is kinetic impact. The missile uses an active Ka-band radar seeker for terminal homing, allowing engagement of tactical ballistic missiles (TBM), cruise missiles, and advanced aircraft. MSE extends range and ceiling beyond the baseline PAC-3 configuration.

ParameterPAC-3 MSE Data
Length5.2 m
Launch weight~316 kg
Kill mechanismHit-to-kill kinetic impact; lethality enhancer collar (focused fragmentation, low NEQ). No main explosive warhead. HD 1.4 for transport purposes.
NEQLethality enhancer only; total energetic content significantly below 1 kg TNT equivalent (estimated). Classified precise figure.
SeekerActive Ka-band (26.5–40 GHz) radar; autonomous terminal homing
PropulsionTwo-stage solid rocket motor; first stage provides boost, second sustains intercept trajectory
Intercept altitudeUp to 40+ km
Intercept range vs TBM~35 km
Intercept range vs aircraft/CM~60 km
Probability of kill (Pk)DATA GAP: campaign-specific Pk figures are classified. Pre-campaign modelling assumed single-shot Pk of 0.80–0.90 vs TBM in benign EW environment.
Rounds per launcher16 (canisterised; M903 launcher)
ProducerLockheed Martin, Camden, AR
Pre-surge production rate~500 rounds per year (open-source estimate; FY24 contract language implies surge to ~700+)
Unit cost (FY25)~USD 5.9–6.2 million per round
Key SRM supplierAerojet Rocketdyne (Camden, AR solid motor facility)
WOME NOTE — Multi-Shot Doctrine: Iranian ballistic missile salvo tactics, as documented across 2024–2025 exchanges, required two to four PAC-3 MSE rounds per inbound TBM to achieve acceptable aggregate Pk against a mixed salvo. At two rounds per target and 1,500–2,000 total AMD interceptors expended, the campaign engaged between 375 and 1,000 discrete inbound TBM/CM threats with PAC-3 and THAAD combined — consistent with reported Iranian ballistic missile sortie rates.

Terminal High Altitude Area Defense (THAAD) Interceptor

THAAD provides upper-tier AMD, engaging TBMs in the terminal descent phase at altitudes between 40 and 150 km. The THAAD interceptor is a pure hit-to-kill system carrying no explosive payload whatsoever; the kill vehicle destroys the target through hypervelocity kinetic impact at closing speeds typically exceeding 2 km/s. THAAD is cued by the AN/TPY-2 X-band radar, which can operate in forward-based mode to extend radar horizon. The low annual production rate of THAAD interceptors makes it the most strategically sensitive of the four depleted systems.

ParameterTHAAD Interceptor Data
Length6.17 m
Launch weight~900 kg
Kill mechanismHit-to-kill kinetic impact only. No warhead. No explosive fill. No NEQ. HD 1.4 (booster propellant only).
PropulsionSingle-stage solid rocket motor (throttleable); Aerojet Rocketdyne
Intercept altitude40–150 km (endo- and exo-atmospheric engagement envelope)
Intercept range~200 km (defended area footprint)
Rounds per launcher8 (canisterised; M1120 launcher)
Fire controlAN/TPY-2 X-band radar; THAAD Fire Control and Communications (TFCC)
ProducerLockheed Martin Space, Sunnyvale, CA (kill vehicle); Camden, AR (booster)
Pre-surge production rate~70–120 interceptors per year (open-source estimate; lowest of any major AMD programme)
Unit cost (FY25)~USD 12–14 million per interceptor
Rebuild timeline at current rateSignificant depletion recoverable over 3–6 years; surge tooling and SRM capacity constrained
DATA GAP: US THAAD interceptor stockpile total is classified. Open-source production estimates suggest a total inventory in the low hundreds. Expenditure of even 50–100 rounds during the campaign would represent a material percentage depletion. CSIS does not name THAAD specifically in the public extract as one of the four “above 50%” systems, but neither does it exclude it.

Industrial Base Analysis: The Solid Rocket Motor Choke Point

All four of the most-depleted munitions — TLAM (booster), PrSM, PAC-3 MSE, and THAAD — share dependence on solid rocket motors (SRMs) manufactured at a small number of US facilities. The SRM supply chain is the principal industrial-base constraint limiting surge production across the portfolio simultaneously. Key facilities include Aerojet Rocketdyne at Camden, Arkansas (PAC-3 MSE and THAAD motors); Northrop Grumman Propulsion Systems at Elkton, Maryland and Rocket Center, West Virginia; and Atlantic Research Corporation. Each facility operates under safety-case-governed energetic material handling constraints that restrict throughput expansion without capital-intensive facility upgrades or new construction.

The strategic implication is that accelerating production of multiple depleted systems concurrently will produce SRM competition for the same sub-tier suppliers. The Munitions Acceleration Council and Pentagon energetics offices flagged this constraint repeatedly through 2025–26, and the FY27 budget request includes investment specifically targeting SRM sub-tier expansion — but new energetics manufacturing capacity takes three to five years to qualify and certify under AOP-7 Edition 3 and equivalent national doctrine.

Expenditure Rate vs Production Rate: Quantitative Assessment

The table below compares estimated open-source production rates against the campaign’s implied minimum expenditure, illustrating the rebuild timeline challenge. All figures are open-source estimates; classified actuals may differ materially.

System Est. Pre-Surge Production (rounds/yr) Campaign Expenditure (minimum estimate) Years to Replace at Pre-Surge Rate
BGM-109 TLAM (all blocks) 150–200 >1,000 5–7 years
PAC-3 MSE ~500 DATA GAP (component of 1,500–2,000 AMD total) DATA GAP; estimated 2–4 years at pre-surge rate
THAAD Interceptor ~70–120 DATA GAP 3–6 years even at modest expenditure
PrSM Block I Ramp-up; classified DATA GAP DATA GAP

Personnel, Safety and EOD Implications

For ammunition technicians (ATs), armament technicians, and EOD operators, the post-campaign inventory reset generates several immediate and medium-term considerations.

Lot-rotation compression. The inventory drawdown compresses lot-rotation cycles. Surge-rate production will introduce a higher proportion of recently manufactured lots with shorter accumulated surveillance histories. ATs should anticipate more frequent acceptance inspections, tighter lot-traceability requirements, and a greater proportion of energetic fills without a long-duration performance baseline. Compliance with DSA 03.OME (formerly JSP 482, now withdrawn) and equivalent national doctrine is mandatory throughout the surge cycle.

Unexploded ordnance (UXO) and dud rounds. At documented campaign expenditure scales, a percentage of rounds will have failed to function as designed. EOD planners and battlefield clearance units operating in or near the Iran campaign area should anticipate dud TLAMs (subsonic, turbofan-sustained; fuze state uncertain on impact), dud PrSM rounds (SRM-driven; potentially armed warhead in failed detonation state), and expended THAAD and PAC-3 MSE kill vehicles (minimal energetic risk; primary hazard is physical damage and propellant residue). The HD and Compatibility Group (CG) re-baselining requirements for new-lot surge production should be completed before those rounds enter forward stockpiles.

Hazard classification during surge transport. TLAM WDU-36/B warhead sections are HD 1.1 CG D. During surge production and acceptance movements, ATs should expect increased tempo of Class 1.1 consignments on supply routes and in ammunition storage facilities (ASFs). Quantity–distance (QD) constraints under STANAG 4439, AOP-7 Edition 3 and relevant national legislation (ADR/RID by road/rail; IMDG Code by sea) must be applied without reduction for operational tempo pressure.

Fuze states in unexpended recovered rounds. Any TLAMs recovered intact (e.g., from failed launch or emergency safing after sortie cancellation) require formal EOD assessment of fuze state before handling. The WDU-36/B warhead uses an FMU-148/B fuze; armed-state confirmation requires specialist AT or EOD assessment. Under no circumstances should recovered intact cruise missiles be handled by non-specialist personnel.

Regulatory and Standards Implications

The surge production and accelerated acceptance of seven munition types simultaneously will generate an elevated tempo of regulatory engagement between prime contractors and national safety authorities. Key regulatory touchpoints include STANAG 4439 (Policy for Introduction and Assessment of New Munitions), which requires safety assessment for any variant change introduced during surge; AOP-7 Edition 3 (NATO Guidelines for the Safety and Suitability for Service Assessment of Munitions), applicable to allied nations receiving US-manufactured rounds; and DSA 02.OME, which governs UK munitions safety case obligations for US-origin munitions entering British stockpiles under materiel-sharing arrangements. The Holston Army Ammunition Plant single-source dependency for RDX and HMX — identified as a critical vulnerability in post-campaign analyses of earlier expenditure rates — remains unresolved and applies to multiple warhead fills across the seven CSIS-assessed systems.

WOME Technical Data Gaps

Authoritative and Editorial References (A&ER)

  1. Center for Strategic and International Studies (CSIS), Last Rounds? Status of Key Munitions at the Iran War Ceasefire, April 2026. csis.org. Source reliability: A / Accuracy: 2 (STANAG 2022).
  2. Raytheon Technologies / RTX Corporation, BGM-109 Tomahawk programme data. rtx.com.
  3. Lockheed Martin, PAC-3 MSE programme datasheet. lockheedmartin.com.
  4. Lockheed Martin, THAAD system overview. lockheedmartin.com.
  5. Lockheed Martin, Precision Strike Missile programme. lockheedmartin.com.
  6. NATO Standardization Office, AOP-7 Edition 3: NATO Guidelines for the Safety and Suitability for Service Assessment of Munitions. Brussels: NSO, 2020.
  7. NATO Standardization Office, STANAG 4439 Edition 3: Policy for Introduction and Assessment of New Munitions. Brussels: NSO.
  8. Defence Safety Authority (DSA), DSA 03.OME: Ordnance, Munitions and Explosives — Regulations. UK MoD. [Successor to JSP 482, now withdrawn.]
  9. DVIDS asset 8189235 — THAAD Deployment, U.S. Army, January 2024. dvidshub.net. Public domain (17 U.S.C. § 105). Reused for editorial purposes with non-endorsement disclaimer.

AI-assisted WOME technical assessment based entirely on open-source material. Not a formal intelligence product. Classification: Open Source / Unclassified. Source reliability: A (CSIS) / Accuracy: 2 (Probably true — awaiting full CSIS data tables and official US production disclosures) under NATO STANAG 2022. All weapon system specifications derived from manufacturer open-source datasheets and published academic/defence analysis; classified figures are identified as DATA GAP throughout.

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