DOD 4120.15-L - Addendum
MDS Designators allocated after 19 August 1998 (until December 2007)
HTML formatting Copyright © 2002-2008 Andreas Parsch
This file lists all MDS designations allocated between 19 August 1998, the "deadline" for the October 1998 release of DOD 4120.15-L (DOD's official list of aircraft and missile designations), and December 2007. The data was acquired by the author from official DOD sources. All designations are presented here in the same format as in DOD 4120.15-L, and are ordered in their "canonical" sequence (sorted by primary mission/vehicle type letter, design number and series letter).
After October 1998, DOD did not publish an updated 4120.15-L file for almost six years (instead of the usual 2-3 year interval). To provide a public reference for new MDS allocations since 1998, new assignments were requested from DOD via the Freedom Of Information Act. The first FOIA request (in early 2002) yielded a list of 72 designations in total, apparently ordered roughly by date of allocation. The index of the entry in this list is shown in parentheses in the "Date/(Index)" column. Follow-up requests yielded more designations, including a small (intended) overlap with the previous set (4 entries). For these designations the date of allocation was also provided, and that is quoted in the first column in place of the simple sequential index for the earlier designations.
Some designations, including all newly assigned design numbers, are further identified in end notes.
This list will be retained although the new 2004 edition of DOD 4120.15-L is now available online (and also includes the new allocations up to early 2004). However, the official document doesn't show the date of allocation for each MDS, has some flaws in the way the data is presented, and of course does not provide explanative notes. Also, this file will be continually updated semi-annually (as long as the FOIA requests are being answered, of course) while DOD 4120.15-L will be updated in the future only once every 2-3 years at best.
Note: At the time of this writing, no official data on MDS designations assigned after December 2007 is available. Newer designations (as well as older ones which for unknown reasons are missing in DOD 4120.15-L), which are confirmed by reasonably reliable sources as being official DOD designations (or soon to be so), are shown in blue entries. Of course, all data in these lines is not official DOD wording. A few designations, which have been used by the military or the industry, but which are not confirmed as official allocations, are shown in light gray.
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 12-Apr-04 | A-10C | Fairchild-Hiller | 2 TF34-GE-100 | AF | Upgraded A-10A to employ smart weapons, digital stores management, and targeting pod. |
| 12-Apr-04 | OA-10C | Fairchild-Hiller | 2 TF34-GE-100 | AF | A-10C aircraft re-roled to fulfill the Forward Air Control (FAC) mission. |
| 12-Apr-04 | FA-18E | McDonnell Douglas / Northrop | 2 F414-GE-400 | Navy | Third major variant of the FA-18 family of aircraft. This is approximately 25 percent larger, but contains 42 percent fewer structural parts than the FA-18C. |
| 12-Apr-04 | FA-18F | McDonnell Douglas / Northrop | 2 F414-GE-400 | Navy | Two-seat version of the FA-18E. |
| 17-May-04 | EA-18G | McDonnell Douglas | 2 F414-GE-400 | Navy | Fourth major variant of the FA-18 family of aircraft. The Electronic Attack version of the FA-18F will serve as the Navy's replacement for the EA-6B providing a capability to detect, identify, locate and suppress hostile emitters. |
| 21-Feb-07 | NEA-18G | Boeing | 2 F414-GE-400 | USN | A permanently modified version of the EA-18G for special testing. [Note NEA-18G] |
| Date (Index) |
Designation | Manufacturer | Engine Data | Department | Description |
| 01-Nov-02 | C-5M | Lockheed Martin | 4 CF6-80C2L1F | AF | Aircraft modified with the Avionics Modernization Program with a digital glass cockpit. |
| 25-Sep-03 | NC-12B | Beech | 2 PT6A-41 | Navy | UC-12B aircraft buno 161311 configured with four P-3C sonobuoy launchers |
| (23) | C-12T | Beech | 2 PT-6A-42 | Army | Complete cockpit configuration change and update. Meets global air traffic management directives. |
| (58) | C-12U | Beech | 2 PT-6A-42 | Army | Complete cockpit configuration change from C-12F. Meets global air traffic management directives. |
| 24-Jun-05 | C-12V | Beech | 2 PT-6A-42 | US Army | A modified version of the C-12R. A short range transport with significant redesign of the cockpit, including console display, dual FMS 3000 GPS navigation, TCAS II air traffic warning system, and Terrain Avoidance Warning System. |
| 17-May-02 | C-23C | Short Bros. Ltd. | 2 PT6A-65AR | Army | Modified C-23B aircraft with cockpit upgrade for compliance with global air traffic management (GATM) requirements. |
| 02-Jun-05 | RC-26B | Swearingen / Fairchild | 2 TPE331-12UA-701G | Air National Guard | A reconnaissance version of the C-26B. It is a short/medium range, medium altitude airborne intel, surveillance (day or night), and recon (tracking and photo) platform allowing full integration into civilian law enforcement. |
| 28-Nov-06 | C-26E | Swearingen / Fairchild | 2 TPE331-12UA-701G | Army | A modified version of the C-26B. A medium range support transport with significant redesign of the cockpit, including console instrument displays, dual FMS 3000 GPS integration, and other mods. Will meet future GATM requirements. |
| 2008 | C-27B | Lockheed Martin / Alenia | 2 RR AE2100-D2 | AF/Army | Model C-27J Spartan, winner of the Air Force/Army JCA (Joint Cargo Aircraft) competition. |
| 07-Nov-02 | C-32B | Boeing | 2 | AF | Mission support aircraft used to meet transportation requirements of government agencies. |
| (5) | UC-35C | Cessna Aircraft Co. | 2 Pratt & Whitney JT15D-5D | US Navy | Upgraded communication and navigation systems and enhanced ground proximity warning systems. |
| (34) | UC-35D | Cessna | 2 Pratt & Whitney 535A | Navy | Cessna Encore version with enhanced ground proximity warning system and enhanced comm/nav equipment. |
| 22-Apr-04 | C-37B | Gulfstream | 2 BR700-710C4-11 | USAF | The Gulfstream G550 aircraft is a 14-passenger, 5-crew executive jet used to support the ROSA VIP/SAM mission. |
| (39) | C-40B | Boeing | 2 CFM65-7B27/B3 | Air Force | Modified C-40A to include distinguished visitor compartment and communications system operator workstation. |
| (40) | C-40C | Boeing | 2 CFM65-7B27/B3 | Air National Guard | Modified C-40A to include convertible cargo area. May be converted for medevac, passenger transport or distinguished visitor. |
| (38) | C-41A | CASA Spain | 2 Garrett TPE 331-10R | Air Force | A light multi-purpose transport capable of high frequency day and night operation, mainly from secondary airfields. Unpressurized aircraft with non-retractable tricycle landing gear. [Note C-41A] |
| 24-Nov-06 | KC-45A | TBD | TBD | Air Force | This MDS was assigned to the KC-X program, as directed by the Chief of Staff of the U.S. Air Force. [Note KC-45A] |
| 17-Oct-05 | NC-130F | Lockheed | 4 T56-A-16 | USN | A modified KC-130F for a Permanent Test Station platform. Mods include range surveillance and clearance, aerial target carriage and launch, and target command and control mission capabilities. |
| 07-Feb-02 | TC-130H | Lockheed Martin | 4 T56-15 | Air Force | Used as pilot proficiency trainer only. |
| 05-Jan-04 (07-Feb-02) |
C-130J (CC-130J) |
Lockheed Martin | 4 AE2100D3 | Air National Guard | Identical to the other C-130J except that it is 180 inches longer and has more switches and locks in the enhanced cargo handling
system. Previously designated CC-130J. [Note C-130J/CC-130J] |
| 25-Oct-05 | KC-130J | Lockheed Martin | 4 AE2100D3 | USN | A modified C-130J for aerial refueling and transport. |
| 16-Jun-06 | MC-130W | Lockheed Martin | 4 T56-A-15 | USAF | A modified version of the MC-130H. Performs night, clandestine low-level, formation aerial refueling of SOF aircraft, forward arming, refueling point, ground refueling ops, resupply, infiltration and psychological warfare missions. |
| 25-Aug-04 | NKC-135B | Boeing | 4 TF33-P9 | USAF/Army | KC-135B modified with a special electronics suite to support USAF and US Army tests. |
| (8) | WC-135C | Boeing | 4 Pratt & Whitney TF33-P-9 | Air Force | Modified EC-135C, serial #62-3582, for atmospheric and meteorological sampling mission. |
| (11) | NC-135W | Boeing | 4 TF33-P-5 | Air Force | Test aircraft used to evaluate, operate, and develop engineering equipment and systems for installation on reconnaissance aircraft. |
| 15-Dec-05 | C-143A | Bombardier | 2 GE CF34-3B | USCG | Twin-engine turbofan aircraft, which will be used for mediumrange command and control support exclusively for the Secretary, Department of Homeland Security and the US Coast Guard Commandant. [Note C-143A] |
| 28-Nov-06 | HC-144A | EADS-CASA | 2 GE CT7-9C3 | USCG | Twin-engine turboprop aircraft used for Search/Rescue/MEDEVAC and cargo. Replacement for the HU-25 family of aircraft. [Note HC-144A] |
| 15-Aug-02 | KC-767A | Boeing | 2 CF6-80C2B7F | AF | Commercial Derivative Air Refueling Aircraft able to offload fuel via boom and drogue. [Note KC-767A] |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 18-Dec-02 | MD-1A | General Atomics | 1 | AF | Control station used to launch, control and recover RQ-1A, MQ-1A, and MQ-9A air vehicles. |
| 10-Jan-03 | MD-1B | General Atomics | 1 | AF | Launch and Recovery Control Station (LRCS) used to launch and recover RQ-1, MQ-1, and MQ-9 vehicles. |
| 11-Feb-05 | MD-1C | General Atomics | N/A | USAF | Containerized Dual Control Station (CDCS) used to launch and recover RQ-1 and MQ-1 air vehicles. The CDCS transfers air vehicle control to a fully functional control station after launch in support of reach-back capability. |
| 30-Mar-05 | MD-1D | General Atomics | N/A | USAF | A multi-aircraft control segment used to control MQ-1 air vehicles. One pilot and four sensor operators can control up to four air vehicles simultaneously. |
| 10-Feb-03 | RD-2A | Northrop | 1 | AF/Navy | Mission Control (MCE), a non-line of sight control station used to launch and recover RQ-4 air vehicles. |
| 29-Apr-04 | YRD-2A | Northrop Grumman | AF | Prototype of the RD-2A Mission Control Element (MCE). Significant modifications and design modernizations will be evaluated for the design, performance, and production of the control segment. | |
| 10-Feb-03 | RD-2B | Northrop Grumman | 1 | AF | Launch Recovery Element (LRE) - a line of sight control station used to launch and recover RQ-4 air vehicles. |
| 29-Apr-04 | YRD-2B | Northrop Grumman | AF | Prototype of the RD-2B Launch and Recovery Element (LRE). Significant modifications and design modernizations will be evaluated for the design, performance, and production of the control segment. |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 19-Jul-04 | E-2D | Grumman | 2 T56-A-427 | Navy | Upgrade of the E-2C with Littoral Surveillance and Theater Air and Missile Defense (TAMD) radar, tactical cockpit, and other system enhancements to operate in both open-ocean and over-land environments against current and projected threats in these environments. [Note E-2D] |
| 27-Sep-05 | E-3G | Boeing | 4 TF33-PW-100A | USAF | A modified version of the E-3B and E-3C vehicles. Modified with advanced mission systems, radar, electronic support measures, internal communications, and mission computers and displays. [Note E-3G] |
| 02-Jan-03 | E-10A | Boeing | 2 TBD | AF | The multi-sensor Command and control aircraft. [Note E-10A] |
| E-10B | Boeing | 2 | AF | MC2A with AMTI (Air Moving Target Indicator) radar system for AWACS role. | |
| E-10C | Boeing | 2 | AF | MC2A with "Rivet Joint" SIGINT sensors. |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 13-Aug-04 | F-5N | Northrop | 2 J85-GE-21 | USN | Upgraded F-5E avionics and equipment for Adversarial program, including radar warning receivers and altimeters, chaff and flares, anti-skid brakes, and upgraded J85-GE-21 engines. |
| 30-Jul-07 | QF-16A | Lockheed Martin | 1 F100-PW-200 | USAF/USN | Air superiority target - a full scale aerial target replacement for the QF-4. |
| 30-Jul-07 | QF-16C | Lockheed Martin | 1 F100-PW-200 | USAF/USN | Air superiority target - a full scale aerial target replacement for the QF-4. |
| Dec 2003 | F-16E | Lockheed Martin | 1 F110-GE-132 | (export) | Formerly known as F-16C Block 60. |
| Dec 2003 | F-16F | Lockheed Martin | 1 F110-GE-132 | (export) | Formerly known as F-16D Block 60. |
| 15-Dec-05 | F-22A | Lockheed Martin / Boeing | 2 F119-PW-100 | USAF | This letter rescinds the approval of FA-22A and FB-22A as directed by the Chief of Staff of the USAF and returns to the F-22A designation. [Note F-22A] |
| 23-Sep-02 | FA-22A | Lockheed Martin | 2 F119-PW-100 | AF | Attack version of F-22A. Single seat model. [Note F-22A] |
| 23-Sep-02 | FB-22A | Lockheed Martin | 2 F119-PW-100 | AF | Bomber version of F-22B. Dual seat model. [Note F-22A] |
| 05-Jun-02 | F-35A | Lockheed Martin | 1 F135-PW-100 or 1 F136-GE-100 |
AF | Next generation strike aircraft for conventional take off and landing. [Note F-35] |
| 05-Jun-02 | F-35B | Lockheed Martin | 1 F135-PW-600 or 1 F136-GE-600 |
Marine Corps | Next generation strike fighter aircraft for Short Take Off and Landing (STOL) version. [Note F-35] |
| 05-Jun-02 | F-35C | Lockheed Martin | 1 F135-PW-400 or 1 F136-GE-400 |
Navy | Next generation fighter for aircraft carrier suitable version. [Note F-35] |
| 25-Aug-04 | YF-117A | Lockheed Martin / Raytheon | 2 F404-GE-F1D2 | USAF | Primary strategic attack aircraft for penetrating high-threat target areas with precision weapons and is the only stealthy, true precision capability currently in the Global Strike Task Force. |
| Date (Index) |
Designation | Manufacturer | Engine Data | Department | Description |
| 10-Apr-02 | TG-10B | Let Flugzeugwerk | none | AF | All metal, 2 seat self supporting high winged glider. Upgraded instrument panel and different cockpit layout from TG-10A. [Note TG-10] |
| 10-Apr-02 | TG-10C | Let Flugzeugwerk | none | AF | All metal, 2 seat, high wing, conventional tail sailplane. Upgraded instrument panel and different cockpit layout from TG-10A. [Note TG-10] |
| 10-Apr-02 | TG-10D | Let Flugzeugwerk | none | AF | All metal, single seat, cantilever mid-high wing, fixed gear and cantilever T-tail sailplane. Upgraded instrument panel and different cockpit layout from TG-10A. [Note TG-10] |
| (28) | TG-12A | Caproni Vizzola/1972 | none | Air Force | Metal/fiberglass, side-by-side high performance glider of cantilever mid-wing monoplane design having a trapezoid rectangular planform of 43:1 aspect ratio. [Note TG-12A] |
| 10-Apr-02 | TG-14A | Grupo Aeromot | 1 Rotax 912 | AF | A two-place, side by side motorglider. It has a T-tail design equipped with a mechanical main landing gear and spoilers on he wing's upper surfaces. [Note TG-14A] |
| 19-Mar-04 | TG-15A | Schempp-Hirth | none | AF | USAF Academy dual-seat Schempp-Hirth "Duo Discus" competition and training glider. [Note TG-15] |
| 19-Mar-04 | TG-15B | Schempp-Hirth | none | AF | USAF Academy single-seat Schempp-Hirth "Discus 2b" competition and training glider. [Note TG-15] |
| Date (Index) |
Designation | Manufacturer | Engine Data | Department | Description |
| 07-Mar-05 | TH-1H | Bell | 1 T53-L-703 | USAF | Modified UH-1H for the Specialized Undergraduate Pilot Training-Helicopter (SUPT-H) program with a dual cockpit configuration. Modifications include: tail boom, main and tail rotator drive components, trasmission, and others. |
| 22-Aug-02 | NAH-1Z | Bell Helicopter | 2 T700-GE-701C | Navy | Permanent special test. |
| 20-Jul-06 | HH-46D | Boeing | 2 T58-GE-402 | USN/USMC | A modified version of the HH-46A for search, rescue, and MEDEVAC missions. |
| 16-Aug-06 | HH-46E | Boeing | 2 T58-GE-16/-16A | USN/USMC | A modified version of the CH-46E for search, rescue, and MEDEVAC missions. |
| 02-May-05 | MH-47G | Boeing | 2 T55-GA-714A | US Army | Upgraded MH-47E for use in Special Operations. Upgrade includes improved engines and incoporation of an infrared exhaust supression system to reduce infrared signatures. Includes additional airframe and electronic upgrades. |
| Dec 2005 | CH-53K | Sikorsky | 3 TBD | MC | Major redesign of CH-53E. Has a wider fuselage (one foot wider in the cabin), sponsons instead of external tanks, larger windscreens, glass cockpit, and new composite rotors. |
| Dec 2005 | YCH-53K | Sikorsky | 3 TBD | MC | Prototype CH-53K for EMD (Engineering & Manufacturing Development). |
| 03-Nov-04 | ZCH-53K | Sikorsky | 3 TBD | MC | Planning stages of the CH-53E redesign. The new design will extend airframe fatigue life, enhance range and lift performance, and improve handling and interoperability. |
| Jan 2007 | TH-57D | Bell | 1 Allison 250-C20BJ | US Navy | Upgrade of TH-57B and TH-57C to common standard with new digital cockpit. |
| 25-Sep-03 | NSH-60F | Sikorsky | 2 T700-GE-401 | Navy | Modified to incorporate a new cockpit layout to support the VH-60N Cockpit Upgrade Program. |
| Dec 2004 | MH-60J | Sikorsky | 2 T700-GE-401C | Coast Guard | HH-60J modified with AUF (Airborne Use of Force) package |
| (44) | HH-60L | Sikorsky | 2 T700-GE-701C | Army | Modified UH-60L with medical mission equipment. |
| 15-Jul-02 | EUH-60L | Sikorsky | 2 T700-GE-701C | Army | Modified with additional mission electronic equipment for Army Airborne Command and Control. |
| (60) | HH-60M | Sikorsky | 2 T700-GE-701C | Army | Modified UH-60A with medical mission equipment. |
| 17-Feb-06 | MH-60M | Sikorsky | 2 CT7-8B5 | Army | A modified version of the UH-60M. Medium and utility support for special operation force unique missions. |
| (50) | MH-60R | Sikorsky | 2 T700-GE-401C | Navy | Modified SH-60B. |
| 22-Aug-02 | YMH-60R | Sikorsky | 2 T700-GE-401C | Navy | Used as prototype. |
| (64) | NSH-60R | Sikorsky | 2 T700-GE-701C | Navy | Used for special testing. |
| (48) | MH-60S | Sikorsky | 2 T700-GE-401C | Navy | Medevac and ship replenishment. Replacing H-46D. |
| 13-Aug-04 | HH-60T | Sikorsky | 2 T700-GE-401C | USCG | Upgraded HH-60J. Modified cockpit and avionics suite with weather search and Forward-looking Infrared Radar(FLIR). A medium range, multi-use, all weather Instructment Flight Rules (IFR) certified vehicle. |
| Dec 2004 | MH-60T | Sikorsky | 2 T700-GE-401C | Coast Guard | HH-60T modified with AUF (Airborne Use of Force) package |
| (32) | HH-65B | Aerospace Helicopter | 2 LTS-101-750 | Coast Guard | Enhanced cockpit configuration and avionics upgrade. |
| (33) | HH-65C | Aerospace Helicopter | 2 LTS-101-750 | Coast Guard | Avionics upgrade and Allied Signal's full authority digital engine control system. |
| 30-Oct-07 | MH-65C | American Eurocopter | 2 Turbomeca Arriel 2C2 | USCG | A modified version of the HH-65C. Modifications include the addition of Airborne Use of Force (AUF) equipment with Counter Drug and coastal security mission capability. |
| (45) | MH-68A | Agusta | 2 P&W PW206C | US Coast Guard | Light twin helicopter used for law enforcement/counter drug operations. [Note MH-68A] |
| 21-Feb-06 | YRH-70A | Bell | 1 Honeywell HTS-900 | US Army | Prototype single engine, single rotor, dual pilot reconnaissance helicopter scheduled to replace the OH-58D Kiowa Warrior. [Note YRH-70A] |
| 2007 | ARH-70A | Bell | 1 Honeywell HTS-900 | US Army | Single engine, single rotor, dual pilot reconnaissance helicopter scheduled to replace the OH-58D Kiowa Warrior. |
| 07-Jul-05 | VH-71A | Lockheed Martin | 3 G.E. CT7-8E | US Navy | One 5-blade main rotor and one 4-blade tail rotor Lockheed-Martin Systems Integration US-101 used for the Presidential Transport mission. [Note VH-71A] |
| 05-Sep-06 | UH-72A | EADS North America | 2 ARRIEL 1E2 | US Army | Lightweight, commercial/non-developmental, single rotor, utility helicopter used for support and security, MEDEVAC, disaster relief, and counter drug operations. [Note UH-72A] |
| Date (Index) |
Designation | Manufacturer | Engine Data | Department | Description |
| (7) | CATM-9X | Raytheon | inert | Navy/Air Force | Used for pilot training in aerial target acquisition and use of aircraft controls and displays. |
| (6) | DATM-9X | Raytheon | inert | Navy/Air Force | Used to train ground personnel in loading, handling and storage. All components inert. |
| (63) | NATM-9X | Raytheon | (no data) | Navy/Air Force | Telemetry system replaces warhead allowing transmittance of missile electrical functions to ground stations during flight. |
| 20-Oct-04 | CATM-65H | Raytheon | n/a | USAF | The CATM-65H training missile is a modified version of the AGM-65H. This Missile performs all functions of an AGM-65H except for launching, and there is no rocket motor installed. |
| (19) | AGM-65K | Hughes | 1 SR114-TC-1 | US Air Force | Improved television guidance and control section |
| (42) | CATM-65K | Raytheon | none | Air Force | Captive training version of AGM-65K |
| 10-Apr-02 | BGM-71H | Raytheon | 1 M-114 | Army | Upgraded warhead to armor piercing for penetrating bunkers |
| 21-Feb-07 | BQM-74F | Northrop | 1 J400-WR-405 | USN | Modified BQM-74E |
| Feb 2008 | AGM-84M | Boeing | 1 J402-CA-400 | USN | Harpoon Block III; upgraded AGM-84 with GPS-aided INS guidance, new seeker, and two-way datalink. |
| (13) | DATM-86C | Boeing | inert | Air Force | Missile loading and handling training. Inert. |
| (12) | AGM-86D | Boeing | 1 F107-WR-100 | Air Force | Modified to deliver penetrator warhead |
| 14-Aug-02 | AGM-88D | Texas Instruments | 1 YSR113-TC-1 | AF/Navy | Provides new Global Positioning System and IMU capabilities. |
| 14-Aug-02 | AGM-88E | Science and Applied Tech Inc. | 1 YSR113-TC-1 | Navy | New guidance and control sections. |
| (41) | FIM-92F | Raytheon | (no data) | Army | Modified FIM-92E with enhancements |
| 05-Sep-02 | FIM-92G | Raytheon | 1 | Army | Guided Missile Intercept-Aerial. Upgrade of the FIM-92D. |
| 06-Sep-02 | FIM-92H | Raytheon | 1 | Army | Guided Missile Intercept-Aerial |
| (43) | MIM-104E | Raytheon | TX-486-1 | Army | Improved detection and enhanced lethality |
| 23-Aug-02 | ATM-114B | Lockheed Martin, Rockwell | 1 13202500 | Navy | Helicopter launched training version of the AGM-114B without the warhead. |
| 30-Mar-07 | ATM-114K | Lockheed Martin | 1 Solid Propellant Rocket Motor | USN | A modified training version of the AGM-114K. This missile is capable of being fired from its airborne platform. |
| (9) | AGM-114M | Lockheed Martin | (no data) | US Army | New blast fragmentation warhead. |
| 24-Feb-03 | AGM-114N | Redstone Tech. | 1 M-120E5 | US Army | Guided Missile, Surface Attack. |
| 04-Jan-05 | AGM-114P | Redstone Tech. | 1 M-120E2 or M-120E5 | US Army | Guided Missile, Surface Attack. UAV launched; modified AGM-114K for high altitude operation to analyze positional data from aircraft to locate and destroy armored vehicles and individual hard targets. |
| AIM-120D | Raytheon | 1 Solid | AF/Navy | Enhanced AIM-120C ("P3I Phase 4"). | |
| 07-Mar-07 | CATM-120D | Raytheon | none | USAF/USN | Captive-carry inert training version of the AIM-120D. Will contain guidance section electronics for enhanced aircrew training. |
| 17-May-02 | AGM-130D | Boeing | 1 WPU-9/B | AF | Uses the BLU-118 warhead and FMU-143J/B fuse. |
| (30) | AIM-132A | Matra BAE Dynamics UK | Solid fuel rocket motor (unspecified) | Royal Australian Air Force | Operational version of YAIM-132A. |
| (26) | RTM-139B | Lockheed Martin | MK 114 MOD 0 | Navy | Training version of RUM-139B. |
| (25) | RUM-139B | Lockheed Martin | MK 114 MOD 0 | Navy | Contains warshot MK 46 MOD 5A torpedo. |
| (66) | RTM-139C | Lockheed Martin | MK 114 MOD 0 | Navy | Training version of RUM-139C. |
| (65) | RUM-139C | Lockheed Martin | MK 114 MOD 0 | Navy | Contains warshot MK 54 MOD 0 torpedo. |
| (10) | MGM-140D | Lockheed Martin | (no data) | US Army | Upgraded missile with numerous structural improvements. |
| (59) | MGM-140E | Lockheed Martin | (no data) | US Army | Upgraded MGM-140B with self guidance using GPS and high explosive warhead. |
| 14-Jan-03 | MGM-140F | Lockheed Martin | 1 | Army | The Guided Missile integrates the Guidance, Warhead, the Rocket Motor, Control Section and the electronic batteries. |
| 10-Feb-03 | DMGM-140F | Lockheed Martin | 1 | Army | The Dummy Guided Missile integrates the Guidance, Warhead, the Rocket Motor, Control Section and the electronic batteries. |
| (15) | CATM-142D | Rafael | inert | Air Force | Used for captive missile training. |
| (14) | DATM-142D | Rafael | inert | Air Force | Used for missile ground training. |
| (17) | ATM-142E | Rafael | WPU-14/B | Royal Australian Air Force | Missile training, no warhead. |
| (16) | CATM-142E | Rafael | inert | Royal Australian Air Force | Used for captive missile training. |
| (18) | DATM-142E | Rafael | inert | Royal Australian Air Force | Used for loading and handling training. |
| (46) | AGM-142F | Rafael | 1 WPU-14/B | Israeli Air Force | Clipped wings, I-800 warhead and unique configuration data links. |
| (61) | AGM-142G | Rafael | WPU-14/B | Air Force of Korea | Has CCD seeker with I-800 warhead and software changes for F-4E flight environment. |
| (62) | AGM-142H | Rafael | WPU-14/B | Air Force of Korea | Has Z-seeker with I-800 warhead and software changes for F-4E flight environment. |
| (20) | FGM-148C | Texas Instruments / Martin Marietta | (no data) | Army | Enhancements to the FGM-148B |
| 05-Oct-04 | FGM-148D | Raytheon / Lockheed Martin | 1 Unknown | US Army | Modification of the FGM-148C for FMS customers |
| (35) | AGM-154D | Raytheon | 1 WJ24-8E or 1 J400-WR-104 | Navy | Turbojet version of AGM-154A with increased standoff range. Contains BLU-97/B submunition. |
| (36) | AGM-154E | Raytheon | 1 WJ24-8E or 1 J400-WR-104 | Navy | Turbojet version of AGM-154C with increased standoff range. Includes a Link-16 weapon data terminal permitting in-flight target location updates and target imagery to the aircrew. |
| 05-Mar-02 | RIM-156B | Raytheon | 1 Mark 104 Mod 3 + 1 Mark 72 Mod 1 |
Navy | A SM-2 Block IVA Aegis VLS extended range guided missile. Additional mission asset defense against short range theater ballistic missiles. |
| (29) | DATM-158A | Lockheed Martin | none | Air Force/Navy | Load crew training version. Inert. |
| 08-Jul-02 | AGM-158B | Lockheed Martin | 1 Teledyne | AF/Navy | Enhanced AGM-158A for greatly extended range due to more efficient engine and greater fuel capacity. |
| 15-May-03 | ZADM-160B | TBD | TBD | USAF | Miniature Air Launched Decoy (MALD) is an air launched, jet powered, airborne vehicle. |
| 05-Feb-07 | DATM-160B | Raytheon | none | USAF | Dummy training version of the ADM-160B. A non-flyable load crew inert trainer, which includes all external operational safety devices and functional remote interface box. |
| 30-Mar-07 | ADM-160C | Raytheon | 1 Hamilton Sunstrand TJ-150 | USAF | A modified version of the ADM-160B. The Miniature Air Launched Decoy (MALD) is an air launched, jet powered, airborne missile used to stimulate, decoy, saturate and/or jam Integrated Air Defense Systems. |
| 29-Aug-06 | RIM-161B | Raytheon | 4 Solid Propellant | USN | Modified RIM-161A. Vertical Launch System (VLS), surface-to-exoatmosphere certified round interceptor. |
| 06-Mar-07 | RIM-161C | Raytheon | 4 Solid Propellant | USN | Modified RIM-161B. Vertical Launch System (VLS), surface-to-exoatmosphere certified round interceptor - Mods to warhead: 2-color seeker sensitivity for increased threat discrimination; greater battle space engagement capability. |
| (53) | RIM-162A | Raytheon | MK 143 MOD 0 | Navy | Employs thrust vector control and interfaces with MK 41 guided missile Vertical Launching System. On ships using Aegis weapon system. |
| (54) | RIM-162B | Raytheon | MK 143 MOD 0 | Navy | Employs thrust vector control and interfaces with MK 41 guided missile Vertical Launching System. On ships using NATO Sea Sparrow surface missile system. |
| (55) | RIM-162C | Raytheon | MK 143 MOD 0 | Navy | Employs thrust vector control and interfaces with MK 48 guided missile Vertical Launching System. On ships using NATO Sea Sparrow surface missile system. |
| (56) | RIM-162D | Raytheon | MK 143 MOD 0 | Navy | Employs thrust vector control and interfaces with MK 29 guided missile Vertical Launching System. On ships using NATO Sea Sparrow surface missile system. |
| (57) | MGM-164A | Lockheed Martin | (no data) | Army | Ground launched missile using inertial-guided concept with GPS inputs to deliver 13 BAT submunitions. [Note MGM-164A] |
| (49) | RGM-165A | Raytheon | MK 104 Rocket Motor | Navy | Land Attack Standard Missile for long range support. Uses GPS nav system and height of burst laser sensors for warhead initiation. [Note RGM-165A] |
| 17-Jul-02 | MGM-165A | Lockheed Martin | 1 Solid Propellant | Army | Guided hypervelocity missile for close combat heavy armor/tank destruction. [Note MGM-165A] |
| 07-Oct-02 | MGM-166A | Lockheed Martin | 1 Solid Propellant | Army | Guided hypervelocity missile for close combat heavy armor/tank destruction. [Note MGM-166A] |
| 02-Jan-03 | BQM-167A | Composite Engineering | 1 Microturbo Tri 60-5+ | USAF | Cost effective and affordable aerial target to support the test and evaluation of weapon systems and operational training. [Note BQM-167A] |
| 05-Aug-03 | MGM-168A | Lockheed | 1 13287300 | Army | Guided Missile, Surface Attack. Self-guided missile that impacts at a pre-determined location. [Note MGM-168A] |
| 16-Dec-04 | YAGM-169A | Lockheed Martin | 1 Solid Propellant | US Army/USN | A "Guided Missile, Surface Attack" Joint Common Missile (JCM) designed to replace the Tow 2A, Hellfire, Maverick, and Brimstone missiles. A chemical energy weapon for lethal engagement of armor and other targets. [Note AGM-169A] |
| 16-Dec-04 | CATM-169A | Lockheed Martin | N/A | US Army/USN | An inert captive training version of the AGM-169A |
| 16-Dec-04 | DATM-169A | Lockheed Martin | N/A | US Army/USN | An inert ballast dummy training version of the AGM-169A |
| 07-Jul-05 | MQM-170A | Griffon Aerospace | 1 3W Modellmotor | US Army | A low cost air defense artillery weapon system training target. Line of sight and over the hill operations drone target; designed for destruction during live fire engagements. [Note MQM-170/171] |
| 07-Jul-05 | YMQM-171A | Griffon Aerospace | 1 3W Modellmotor | US Army | A low cost air defense artillery weapon system training target prototype. UHF operations drone target; designed for destruction during live fire engagements. [Note MQM-170/171] |
| 14-Jun-06 | FGM-172A | Lockheed Martin | 1 Solid Propellant | USMC | Shoulder fired, fire and forget, anti-tank missile capable of penetrating explosive reactive armor. [Note FGM-172] |
| 14-Jun-06 | FGM-172B | Lockheed Martin | 1 Solid Propellant | USMC | Shoulder fired, fire and forget, anti-material missile capable of pentrating structures, fortified positions, and light armor. [Note FGM-172] |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 15-Aug-04 | EO-5C | DeHavilland | 4 PT6A-50 Turboprop | US Army | Six Airborne Reconnaissance Low Multifunction (ARL-M) aircraft. Perform low altitude monitoring of communications (COMMINT) signals and has imaging (IMINT) capability and Moving Target Indicator radar. |
| 15-Aug-04 | TO-5C | DeHavilland | 4 PT6A-50 Turboprop | US Army | One Airborne Reconnaissance Low Trainer(ARL-T) aircraft. The trainer has the same modernized cockpit design as the EO-5C, but carries no mission equipment. |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 25-Aug-04 | EP-3E | Lockheed Martin | 4 T56-A-14 | USN | Signals Intelligence (SIGINT) reconnaissance aircraft |
| 30-Mar-05 | P-8A | Boeing | 2 CFM56-7B Turbofan | Navy | Replacement for P-3C Orion. Boeing 737-800ERX airframe to perform anti-submarine and anti-ship mission with ability to deploy weapon systems using hard points on wings and a fuselage internal bomb bay. [Note P-8A] |
| Date (Index) |
Designation | Manufacturer | Engine Data | Department | Description |
| 13-Feb-02 | MQ-1B | General Atomics | 1 Turbocharged Rotax 914 | AF | Medium altitude endurance unmanned aerial vehicle with a deicing wing capability and an internal and external payload capability. Has a multiple role mission. |
| (21) | RQ-1B | General Atomics | Turbocharged Rotax 914 | Air Force | Larger engine, wing deicing and improved avionics. |
| 30-Oct-07 | MQ-1C | General Atomics | 1 Thielert Centurion 1.7 | Army | A replacement for the MQ/RQ-5 family of UCAV/UAV. Provides an extended range and multi-mission capability. Has 36-hour endurance with an 800-pound payload. Has 56-foot wingspan ans 27-foot length. |
| 06-Jul-06 | YMQ-1C | General Atomics | 1 Thielert Centurion 1.7 | Army | A replacement for the MQ/RQ-5 family of UCAV/UAV. Provides an extended range and multi-mission capability. Has 36-hour endurance with an 800-pound payload. Has 56-foot wingspan. [Note YMQ-1C] |
| (22) | RQ-2B | Pioneer Unmanned Aerial Vehicles Inc. | SF-2-350 | Navy/Marines | Improved electronic system requiring different aircrew and maintenance procedures. |
| 07-Feb-07 | RQ-2C | Pioneer UAV | 1 UAV Eng Ltd AR741-38 | USN/USMC | Modified RQ-2B. Tactical UAV designed for day/night ISR operations with take-off and recovery from a hard surface. Mods include AR 741-38 engine and Laser IR pointer to increase the operational combat capability through 2015. |
| 29-Apr-04 | YRQ-4A | Northrop Grumman / Teledyne Ryan | 1 RR AE-3007H | AF | Prototype of the RQ-4A. Significant modifications and design modernizations will be evaluated for the design, performance, and production of the vehicle. |
| 25-Apr-03 | RQ-4B | Northrop | 1 AE-3007H | USAF | Larger, enhanced version of RQ-4 UAV for expanded reconnaissance mission. |
| (1) | RQ-5A | TRW Inc. | 2 Moto Guzzi Motorcycle Engines | US Army | UAV with 8 hour endurance and 15,000 foot ceiling. Has 29 foot wingspan. [Note RQ-5A] |
| 08-Apr-05 | MQ-5A | Northrop Grumman | 2 Moto Guzzi | US Army | Modified RQ-5A for a Multi-mission role. Includes hard-points on each side capable of carrying external payloads and vehicle modifications to facilitate mission. |
| 16-Aug-04 | MQ-5B | Northrop Grumman | 2 Mercedes Benz I80 | US Army | Modified RQ-5A for Reconnaisssance and Attack Missions. Modified engines, new avionics, longer wingspan (from 29 to 34.25FT) to allow for increased gross take-off weight, altitude and longer endurance. |
| (2) | RQ-6A | Alliant Techsystems | 1 UEL 801 Rotary Engine | US Army | UAV with 2-4 hour endurance and 13,000 foot ceiling. Has 13 foot wingspan. [Note RQ-6A] |
| (27) | RQ-7A | AAI Corp. | 1 AR-741 Gas Rotary Engine | Army | Operates at up to 200 kilometers behind front lines at altitudes up to 15,000 feet with 4 hours station duration. Day/night surveillance video sensors supplying near real-time information. [Note RQ-7A] |
| 07-Oct-04 | RQ-7B | AAI Corp. | 1 AR-741-1100 UAV | US Army | Upgraded RQ-7A. Modified AR-741 engine, larger wing, tail, boom. And fuel tanks to allow for reduced loiter speed and longer endurance. A day/night, adverse weather,multisensor collection system for real-time battle information. |
| (47) | RQ-8A | Northrop Grumman / Ryan Aeronautical | 1 Allison 250-C20 | Navy | Provides real-time imagery, target designation. [Note RQ-8A] |
| 24-Jun-05 | MQ-8B | Northrop Grumman / Ryan Aero Center | 1 Allison 250-C20 | US Army | Upgraded RQ-8A. Modified rotor blade, fuel tank, tail assembly, etc. to allow for a multi-mission role with the carrying and firing of ordnance. |
| 01-Feb-02 | MQ-9A | General Atomics | 1 Honeywell 331-10 | Air Force | Medium to high altitude endurance unmanned aerial vehicle. Has a multiple role mission. [Note MQ-9A] |
| 02-Jan-03 | YMQ-9A | General Atomics | 1 Honeywell 331-10 | AF | Prototype configuration of the MQ-9A, a medium/high altitude endurance unmanned aerial vehicle (UAV). |
| 14-Feb-03 | CQ-10A | MMIST Corp. | 1 ROTAX 914 | Army | The drone aircraft employs a Para-foil air canopy, integrated with a commercially developed airborne guidance unit and engine. [Note CQ-10A] |
| 20-Oct-04 | RQ-11A | AeroVironment | 1 Aveox 27/26/7-AV | AF/Army | Hand launched, low/medium altitude, small-UAV used to provide over-the-hill and around-the-corner intelligence, surveillance, and reconnaissance capabilities to ground troops. [Note RQ-11A] |
| 22-Aug-06 | RQ-11B | AeroVironment | 1 Aveox 9100242-02 | AF/Army | A modified version of the RQ-11A. High efficiency, long endurance motor, camera Pan/Tilt/Zoom and increased field of view, and Laser Illuminator. |
| 30-Mar-07 | RQ-14A | AeroVironment | 2 Aveox 1105/6Y Electric Brushless | USN | Hand or bungee launched, low altitude, small-UAV flown autonomously used to provide real time Intelligence, Surveillance, and Reconnaissance (ISR) imagery in support of tactical units. [Note RQ-14A] |
| 30-Mar-07 | RQ-14B | AeroVironment | 2 Aveox 1105/6Y Electric Brushless | USN | A modified version of the RQ-14A. Hand or bungee launched, low altitude, small-UAV flown manually or autonomously used to provide real time Intelligence, Surveillance, and Reconnaissance (ISR) imagery in support of tactical units. |
| 21-Feb-07 | RQ-15A | DRS Unmanned Tech. | 1 LAE-150, 2 Cyl 16-HP Gasoline | USN | Pneumatically container/launched, low/medium altitude, small-UAV to provide Intelligence, Surveillance, and Reconnaissance (ISR) imagery in support of tactical units. Parachute land or water recovery. [Note RQ-15A] |
| 16-May-07 | YRQ-16A | Honeywell | 1 3W-56, 4HP 56cc Bower Twin | US Army | A VTOL Micro-UAV that provides real-time reconnanaissance, surveillance, target acquisition, and battlefield management both day or night. [Note YRQ-16A] |
| 02-Jul-07 | XMQ-17A | MTC Technologies | 1 Honda GX-57 | USMC | Multi-mission day/night unmanned aircraft that serves as a concept demonstrator and test platform for emerging technologies. [Note XMQ-17A] |
| (Index) | Designation | Manufacturer | Engine Data | Department | Description |
| (4) | MS-1A | TBD | TBD | US Air Force | Spaceplane with suborbital flight for multimission space support. [Note MS-1A] |
| (Index) | Designation | Manufacturer | Engine Data | Department | Description |
| (3) | NS-7E | Boeing North America | none | DOD | Sustainment of Global Positioning System |
| 07-Mar-07 | ES-14A | Boeing IADS | none | DOD | High capacity communications satellite used for command, control, and communications. [Note ES-14A] |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 05-Dec-07 | T-6B | Raytheon | 1 PT-6A-68 | USAF/USN | A modified version of the T-6A. Modifications include an Integrated Avionics System including multifunction displays, Integrated Avionics Computers, heads-up display, and structural modification for increased gross weight. |
| 12-May-06 | T-44C | Raytheon | 2 PT-6A-34B | Navy | A modified T-44A. Modifications include digital glass cockpit avionics upgrade to overcome obsolescence and discontinuance of parts enabling continuance of mission support until 2025. |
| 13-Mar-03 | T-48A | TBD | TBD | Navy | A multi-place aircraft used to train flight officers in fundamentals of aviation and communication. [Note T-48A] |
| 18-Jul-03 | CT-49A | Boeing | 4 JT3D-7 | NATO | NATO Trainer-Cargo Aircraft (TCA) operated to support E-3A AWACS training and air transport/cargo for NATO (NAEW&CF). [Note CT-49A] |
| 17-May-05 | T-50A | Korea | MDS RESERVED ON 17 MAY 05 [Note T-50A] | ||
| 07-Jul-05 | T-51A | Cessna | 1 O-320-E2D | USAF | An all-metal, single engine, strut-braced, high wing monoplane. Single engine placed forward of the fuselage centerline and fixed tricycle landing gear. [Note T-51A] |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 27-Sep-05 | U-28A | Pilatus | 1 PT6A-67B | USAF | Single engine turbo-prop utility aircraft (1 to 2 crew, 9-passengers) [Note U-28A] |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 20-Oct-04 | CV-22B | Bell / Boeing | 2 T406-AD-400 | USN | Vertical take-off and landing aircraft used to support special forces. |
| Date (Index) |
Designation | Manufacturer | Engine Data | Department | Description |
| Nov 2006 | X-37B | Boeing | USAF | Orbital Test Vehicle (OTV) for evaluation of reusable military space vehicle technologies and concepts. | |
| (31) | X-40B | Boeing | TBD | DOD | Upgrade using reusable rocket motor, advanced thermal protection systems, avionics and flight control systems. |
| (24) | X-44A | Lockheed Martin / Pratt & Whitney | (no data) | NASA/Air Force | Highly modified F-22A by removing tail, installing delta wings, pitch/yaw low observable nozzles, pneumatic vortex control, and mechanical and fluidic thrust vectoring nozzles. [Note X-44A] |
| (37) | X-45A | Boeing Phantom Works | F124-GA-100 | Air Force | Demonstrate technical feasibility for an unmanned combat air vehicle to prosecute suppression of enemy air defenses and strike missions. [Note X-45A] |
| 02-Jul-03 | X-45B | Boeing | 1 F404-GE-102D | USAF | The X-45B Unmanned Combat Air Vehicle (UCAV) was a demonstrator concept studied from 2001 to 2002 to build on lessons from the X-45A. |
| 02-Jul-03 | X-45C | Boeing | 1 F404-GE-102D | USAF/Army | The X-45C Unmanned Combat Air Vehicle (UCAV) demonstrator builds on lessons from the X-45A. |
| (51) | X-46A | Boeing | Turbofan | Navy | Aircraft carrier based to demonstrate feasibility of unmanned combat air vehicle. [Note X-46A] |
| (52) | X-47A | Northrop Grumman | Turbofan | Navy | Aircraft carrier based to demonstrate feasibility of unmanned combat air vehicle. [Note X-47A] |
| (67) | X-47B | Northrop Grumman | Turbofan | Navy | Full scale version of X-47A. |
| (68) | X-48A | NASA and Boeing | 3 Williams J24-8 | NASA | Blended wing-body low speed vehicle to investigate its stability and control characteristics. Remotely piloted with wingspan of 35 feet and 3,000 pound weight. [Note X-48A] |
| 15-Jun-05 | X-48B | Boeing / Cranfield Space | 2 | NASA/USAF | Blended wing-body, low speed vehicle, used to investigate the stability and control of this aerospace vehicle shape. Remotely piloted vehicle with a wingspan of 20.4 feet and weighing between 284-392 pounds. |
| 23-May-03 | X-49A | Sikorsky and Piasecki | 2 T700-GE-401C | Navy | One SH-60F will be converted to test the feasibility under the advanced technology demonstration (VTDP). [Note X-49A] |
| 13-Feb-02 | X-50A | Boeing Phantom Works | 1 Williams F112 | DARPA/DOD | Canard rotor/wing demonstration vehicle. Aircraft capable of rapid transition between a rotary helicopter, for VTOL operation, and a high speed fixed wing vehicle. [Note X-50A] |
| 27-Sep-05 | X-51A | Boeing / Pratt & Whitney | 1 SJY61-1 | USAF | Hypersonic vehicle to flight test the USAF hypersonic technology scramjet engine in flight from mach 4.5 to 6.5. Self-piloted with overall stack length of 290-inches and with a gross weight of 3772 pounds. [Note X-51A] |
| 16-Aug-06 | X-53A | Boeing | 2 F404-GE-400 | USAF/NASA | Highly modified, experimental F/A-18A to flight test the active aeroelastic wing technology for applications on existing and new aircraft designs. [Note X-53A] |
| Date | Designation | Manufacturer | Engine Data | Department | Description |
| 17-Aug-06 | MZ-3A | ABC | 2 IO-360-BIG6 | USN | Twin-engine Lighter-Than-Air airship used for sensor development, demonstration, and deployment. [Note MZ-3A] |
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