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Request for Information · Response
Counter-Unmanned
Aircraft Systems
C-UAS · Citadel Multi-Domain Interception System
Topic Area — Munition-Ordnance
In response to a Request for Information (RFI)
Department of Homeland Security (DHS)
Science & Technology (S&T) Directorate
Office of Mission and Capability Support (MCS)
RFI 70RSAT26RFI000018
Technical POC
Jacob Lopata
Chief Technology Officer
(312) 252-9770
jacob.lopata@tehiru.systems
175 E. Delaware Place, Chicago, IL 60611
Administrative POC
Aaron Prat
Chief Executive Officer
(213) 281-0860
aaron@tehiru.systems
15 Lily Pond Ct., Rockville, MD 20852
Tehiru Aerial Systems, Inc., a Delaware Corporation, and its subsidiary Tehiru Space Technologies Ltd, an Israeli Corporation (together < 25 employees), qualify as non-traditional defense contractors. NAICS code: 336411 — Unmanned and Robotic Aircraft Manufacturing.
Controlled Unclassified Information (CUI)

This submission contains Controlled Unclassified Information, company-proprietary, and unrestricted information only, and shall not be disclosed outside the Government or used for any purpose other than to evaluate this application. No classified information is included.

Tehiru Aerial Systems, Inc.

Cover Letter

RE: RFI 70RSAT26RFI000018 — C-UAS Kinetic Mitigation Demonstration · Topic Area: Munition — Kinetic Interceptor

To the DHS S&T C-UAS Program Office,

Tehiru Aerial Systems, Inc. respectfully submits this application in response to RFI 70RSAT26RFI000018 for participation in the DHS Science & Technology kinetic sUAS mitigation demonstration. Our submission addresses a single topic area — Munition / Kinetic Interceptor — and presents the Citadel Multi-Domain Counter-UAS Interception System. The following identifying information is provided per Section 3.1.

Company NameTehiru Aerial Systems, Inc.
Company Address15 Lily Pond Ct., Rockville, MD 20852
UEI Number[UEI — INSERT SAM.gov Unique Entity ID]
Size & Socio-Economic Status[CONFIRM — e.g., Small Business under NAICS 332992]; non-traditional defense contractor (Tehiru Aerial Systems, Inc. + subsidiary Tehiru Space Technologies Ltd, together < 25 employees).
Applicable NAICSRFI-designated: 332992 — Small Arms Ammunition Manufacturing (PSC 1095). Corporate primary: 336411 — Unmanned & Robotic Aircraft Manufacturing.
Technical POCJacob Lopata, Chief Technology Officer · (312) 252-9770 · jacob.lopata@tehiru.systems
Contracting POC[CONFIRM Contracting POC — name / title / email / phone] · Administrative: Aaron Prat, CEO · (213) 281-0860 · aaron@tehiru.systems
Contract Vehicles[LIST awardee vehicles (BPA / IDIQ / OTA) + administering agency, or state “None”]
RFI Topic AreaMunition — Kinetic Interceptor (single topic area per submission).
System TitleCitadel Multi-Domain Counter-UAS Interception System
Availability — Nov 2026Yes — demonstrable November 2026 at a CA / FL / NV / OK / TX test range.

Fielding history (last 3 years): Tehiru Aerial Systems has supplied hundreds of autonomous attack drones, under special authorization, to operational units in collaboration with Israel’s Directorate of Defense R&D (Maf’at) and Unit 81. The Citadel interceptor and its guidance/autonomy stack derive from these fielded systems. [CONFIRM any U.S./commercial fielding to list here, if applicable]

This submission is a participation application, not an acquisition proposal. All materials are limited to Controlled Unclassified Information (CUI), company-proprietary, or unrestricted information and are marked accordingly.

Respectfully,

Aaron Prat
Chief Executive Officer · Tehiru Aerial Systems, Inc.

Tehiru Aerial Systems, Inc.

Table of Contents

1   Section 1 — Corporate Expertise1
1.1   Company Background1
1.2   System Description and Capabilities1
1.2.1   Citadel: Multi-Domain Counter-UAS Defense System1
1.2.2   System Components (Hive · SharkOS)1
1.2.2.3   Cipher Interceptor2
1.2.2.4   Availability & Fielding2
2   Section 2 — System Description and Cost Estimate3
2.1   Overview (System Description · Operational Concept)3
2.1.3–2.1.5   TRL · Specifications · Sustainment4
2.1.6–2.1.9   Systems · Laydown · Mobility · Engagement5
2.2   ROM Costs · Regulatory Registration5
2.3   Performance · Requirements vs. Response6
2.3.5   Capabilities-Sought Coverage7
2.4   Demonstration Availability7
Visual Appendix — System ImageryA-1
Tehiru Aerial Systems, Inc.

1 — Corporate Expertise

Citadel interceptor engaging a target
Citadel interceptor on an autonomous intercept run (see Visual Appendix, Fig. A-1).

1.1   Company Background

Founded in 2022 by a team of robotics enthusiasts and UAS technologists, Tehiru Aerial Systems and its subsidiary Tehiru Space Technologies Ltd design and build fully autonomous counter-UAS and counter-ATGM systems at scale with unmatched cost-efficiency. Tehiru is revolutionizing low-altitude, short-range air defense by developing sophisticated communication and autonomy systems that enable intelligent, precision operations with minimal human intervention. Tehiru has supplied hundreds of attack drones, under special authorization, to operational units in collaboration with various military divisions and specialized units — including Israel’s Directorate of Defense R&D (Maf’at) and Unit 81.

1.2   System Description and Capabilities

1.2.1   Citadel: Multi-Domain Counter-UAS Defense System

The Citadel Interception System is a fully autonomous threat-mitigation system designed to provide advanced protection against hostile air attacks. With the ability to counter Group 1–3 UAS, Citadel delivers a reliable, scalable solution for force and point protection. It is a detection-system-agnostic, multi-platform solution deployable across air, land, and sea. On land it installs as a fixed site or on a range of vehicles; at sea it deploys on naval vessels to protect high-value maritime assets. Detection-system integration may be accomplished by Tehiru partners or existing government-designated providers, enabling near plug-and-play operation with the Citadel architecture. (See Visual Appendix, Fig. A-1 — engagement sequence.)

1.2.2   System Components

1.2.2.1   The Hive + Magazine

The Hive is Tehiru’s integrated interceptor management and deployment system, designed to store, sustain, and launch interceptors directly from mobile or fixed platforms across multiple domains. Each Hive houses two interceptors in a hot-swappable magazine for controlled, sequential, rapid deployment, and manages the interceptor energy lifecycle (charging, health monitoring, readiness optimization) so each unit stays mission-ready without manual intervention. The system manages launch sequencing and deployment logic in synchronization with the interceptor’s onboard flight-management systems, transforming host platforms into sustained cUAS defense nodes. A full Citadel interceptor unit consists of two Hives and five magazines: two installed in the Hives (four interceptors launch-ready) and three additional magazines stored and charged in a docking station for rapid reload. (See Visual Appendix, Fig. A-2.)

1.2.2.2   SharkOS

Tehiru’s SharkOS is the distributed engagement and fire-control operating system powering the Citadel cUAS stack. Operating directly on each interceptor, it enables localized guidance, intercept execution, and terminal engagement logic at the edge — supporting scalable defense against multiple simultaneous threats. Each interceptor executes mission logic independently while a ground-based scheduling layer manages tasking, prioritization, and resource allocation, minimizing operator burden and compressing time-to-effect. SharkOS aligns with modular open-systems principles, interfacing with third-party or government-provided detection systems through defined target-state and performance requirements, and operates over fully encrypted, resilient communication pathways in contested, degraded, or sporadic-communication environments.

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Cipher interceptor
Fig. A-3 — Cipher interceptor

1.2.2.3   Cipher Interceptor

Cipher is a modular interceptor drone designed for integration with the Hive platform. As a hardware system it provides the airframe, payload interfaces, and onboard compute required to support SharkOS for mission execution and control. Rather than a single fixed configuration, Cipher can be delivered in multiple variants tailored to customer requirements, with configurable payloads and performance characteristics. (See Visual Appendix, Fig. A-3.)

1.2.2.4   Availability & Fielding

The Citadel Interception System is in advanced development at TRL 6 and is expected to be available for demonstration, as described herein, by November 2026. The interceptor and its guidance/autonomy stack derive from Tehiru systems fielded with Israeli defense units (Maf’at, Unit 81) within the last three years. [CONFIRM any U.S./commercial fielding to add]

TRL 6 — prototype demonstrated in a relevant environment
Tehiru Aerial Systems, Inc.
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2 — System Description & Cost Estimate

Interceptor closing on target
Terminal closure on a fixed-wing sUAS

2.1   Overview

2.1.1   System Description

The Citadel Interception System is a ground-launched, kinetic counter-UAS (cUAS) system designed to detect, track, and neutralize airborne UAS threats. It comprises four principal subsystems: a ground-based detection subsystem, a ground control station (GCS), an autonomous interceptor vehicle, and a kinetic defeat munition (warhead). The system is detection-system agnostic — the Cipher Interceptor integrates with any appropriate ground detection system using radar, LIDAR, EO sensors, or a fusion thereof.

The GCS receives and processes target-state data, monitors the tactical situation, and determines the launch moment based on target range and flight dynamics. Upon the decision to engage, it transmits a launch command with real-time guidance to the interceptor over a dedicated RF uplink. The interceptor — a multi-rotor UAS — executes a fully autonomous, multi-phase interception using onboard edge compute, generating a dynamically updated intercept path and controlling attitude and thrust to close on the target. A secondary RF channel provides an independent manual flight-control link for operator safety override and security contingencies. An onboard proximity-detection system senses the target within 15 m and, at a predetermined time, signals warhead detonation to neutralize the threat.

2.1.2   Operational Concept and Employment

  1. Detection subsystem acquires and tracks a threat UAS (RCS −20 dBsm), continuously transmitting position (x/y/z) and velocity (vx/vy/vz).
  2. GCS evaluates range-to-target against the engagement envelope; when the threat enters it, the GCS initiates intercept via launch command + guidance on the primary RF uplink.
  3. Interceptor executes an autonomous, multi-phase launch sequence adapted to the threat’s state.
  4. Interceptor navigates toward the threat, continuously pursuing it using updated detection-subsystem state data.
  5. At T-3 s to interception, the warhead is armed.
  6. In the terminal phase (<15 m separation), the proximity-detection system signals the electronic safe & arm (ESAD) to detonate and neutralize the threat.
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Hive interior magazine bays
Hive interior — magazine bays (Fig. A-2)

2.1.3   Technology Readiness Level (TRL)

The integrated Citadel system is assessed at TRL 6. The onboard guidance and autonomous- intercept system has been validated through successful intercepts of Group 1 and Group 2 UAS in representative environments; end-to-end validation from detection and ground-station cueing through autonomous intercept has been demonstrated in a relevant environment. The warhead/ESAD and proximity-detection system is in active development at TRL 5.

2.1.4   Pertinent Technical Specifications

A · Interceptor / Effector
  • All-up weight ≈ 1 kg (excl. effector); 5-inch propeller config.
  • Max speed 50 m/s; 6S LiPo (22.2 V, 1.4 Ah, ≈31 Wh).
  • Primary RF 2.4 GHz guidance, ≈5 km; 900 MHz manual RC.
B · GCS  ·  C · Warhead
  • GCS: single NVIDIA Jetson / PC-class unit; real-time monitoring + post-mission analysis.
  • Warhead: total 650–800 g; HE 150–200 g; fragmentation/omnidirectional, cylindrical; electric high-voltage ESAD.

2.1.5   Support / Sustainment Concept

Interceptor — 2 per Hive in a hot-swappable magazine, ready for sequential engagement; expendable, restocked after each engagement; rated −20 °C to +40 °C (storage to +70 °C); stored in-theater in sealed magazines.

Warhead — segregate munitions by type/hazard class/compatibility group; maintain minimum separation distances (storage, personnel, vehicles, fuel, command); limit explosive quantity per location; use berms/revetments/hardened structures; control ignition sources (flame, static, RF emitters, exhaust).

GCS — operates autonomously once engaged, minimal operator intervention; a single operator supervises and activates; operator-level routine maintenance, no on-site technician for day-to-day operation; single flight operator.

Manufacturer — Tehiru provides full lifecycle support (software updates, releases, hardware repair/replacement); updates delivered and managed by Tehiru. Detection subsystem — sustainment by a third-party supplier.

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Hive closed transport configuration
Hive — closed transport state

2.1.6   Number of Systems — Simultaneous Use

One complete system will be fielded — a single Hive, one GCS, and one detection subsystem. The Hive supports single-interceptor engagements; approximately 10 interceptors will be on-site for the demonstration, supporting multiple sequential engagements.

2.1.7   Laydown Configuration

Representative site laydown (sensor, control, and launch element placement) is provided in the Visual Appendix, Fig. A-4.

2.1.8   System Mobility / Transportability

The system supports both mobile and fixed-site deployment — mountable on tactical or armored vehicles for mobile cUAS protection, or installed as a static defense position for bases, critical infrastructure, and protected facilities. The modular design enables rapid deployment and integration across platforms.

2.1.9   Method of Engagement

Citadel integrates with third-party detection/tracking sensors. On detection, target data is relayed to the GCS; interceptor UAVs launch from the modular Hive launcher, enabling rapid sequential or simultaneous engagements. Each interceptor is autonomously guided to a predicted interception point and employs a proximity-based engagement, initiating a controlled detonation at the calculated intercept point — designed for engagement effectiveness within a <70 cm closure distance.

2.2   Rough Order of Magnitude (ROM) Costs

ComponentRough Unit Cost
Interceptor (per effector, expendable)$5,000
Magazine (2-interceptor, hot-swappable)$1,500
Hive (launch / management unit)$20,000

Configurations: a full unit = 2 Hives + 5 magazines (4 launch-ready + 3 reserve); scales by Hive/magazine count; Cipher offered in multiple payload variants. Maintenance & updates: operator-level routine maintenance; full lifecycle support at an estimated [CONFIRM annual maintenance ROM]; software/firmware updates on a [CONFIRM cadence] schedule, with expedited threat-driven releases.

2.2.1 Regulatory Registration: the 2.4 GHz guidance and 900 MHz manual-control links operate under [CONFIRM FCC status — Part 15 / Experimental / pending]; Tehiru will coordinate all spectrum/regulatory approvals with the Government before the demonstration.

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Terminal kinetic defeat
Kinetic defeat at intercept point

2.3   Performance

2.3.1   Coverage Area & Minimum RCS

Detection/tracking coverage extends to ≈3 km radius (≈28 km²). The engagement zone extends to ≈800 m radius at altitudes up to ≈100 m (≈2 km²). Minimum RCS for detection/tracking at max range is −20 dBsm.

2.3.2   Operational Scenarios

The system employs an explosive effector as its sole mitigation method. An autonomous interceptor is launched and guided to the designated threat, neutralized via onboard warhead detonation at intercept. As a kinetic, precision-guided system, it selectively engages a single designated target without affecting other UAS present.

2.3.3   Tracking, Limitations & Integration

Provides 3D tracking for targets with RCS −20 dBsm at speeds >150 m/s. APIs are available for rapid integration with third-party or partner detection systems.

2.3.4   Requirements vs. Response

RequirementTehiru Response
Effective coverage area (km²).Up to 3 km radius, 360° coverage; ≈28.3 km².
Minimum RCS for detection/tracking.−20 dBsm
sUAS detection/tracking range by size.Group 1: 3 km · Group 2: 8 km · Group 3: 15 km (max).
Location accuracy.±2.5 m at maximum range.
Simultaneous detect/track/ID/mitigate.Full Hive battery: up to 4 sUAS simultaneously.
Mitigation type; selective single-target.Explosive effector (sole method); precision guidance enables selective single-target engagement.
Tracking dimensionality.3D radar tracking, hemispherical (360°×50°).
Limitations.Line-of-sight dependent; target within field of view. No limit on drone type/size.
Setup time & manpower.Mobile radar: 3 operators, 45–90 min. Fixed radar: ≈1 day.
Operators required.One operator.
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RequirementTehiru Response
Display / share data with other systems; ingest formats.Laptop display of target position/track data; integration with AiCloud C2, ATAK, NINJA; data exchange via REST, MQTT, ZMQ, and direct-connect APIs.
APIs for external integration.REST, MQTT, ZMQ, Direct-Connect, ATAK, NINJA.
Supporting information.AI object classification, environmental learning, dynamic clutter filtering, multi-radar control, historical track retention, secure remote management, cloud-connected or standalone operation.
Hive open configuration
Hive — open, four-bay layout

2.3.5   Capabilities-Sought Coverage

Capability Sought (RFI §2.3.1)SatisfiedCitadel
Munition — Kinetic InterceptorFullPrimary. Autonomous interceptor + onboard warhead; validated vs. Group 1 & 2.
Munition — OrdnanceFullComplete fragmentation warhead (150–200 g HE, HV ESAD).
Munition — MissilesPartialPowered, externally-guided vehicle; not a rocket-motor missile.
Entanglement (net / fouling)Not offeredKinetic effector only.
Directed EnergyNot offeredNo DE effector.
GNSS Denial · RF Interference · Nav Denial/SpoofingNot offeredDefeats targets kinetically regardless of target navigation/RF.

2.4   Demonstration Availability

The Citadel Interception System will be demonstrable in November 2026 at any of: California, Florida, Nevada, Oklahoma, or Texas (exact site TBD).

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Visual Appendix
System Imagery

Supplementary imagery referenced from Sections 1–2. Provided for context; not counted against section page limits.

Interceptor in flight Interceptor closing on target Terminal detonation
Fig. A-1 — Citadel engagement sequence: interceptor in flight → terminal closure on a fixed-wing sUAS → kinetic defeat.
Hive closed Hive open
Fig. A-2 — The Hive: closed transport state (left) and open state showing the four-bay interior magazine layout (right).
Cipher interceptor
Fig. A-3 — Cipher modular interceptor: quad-rotor airframe with cylindrical warhead payload and onboard compute.
Tehiru Aerial Systems, Inc.
A-1