L’XM312 è una mitragliatrice pesante derivata dall’ XM307 calibro 25 mm, camerata per la cartuccia BMG .50.
È stata progettata in risposta ad una richiesta delle forze armate statunitensi per sostituire la oramai datata ma insostituibile mitragliatrice M2 Browning M2, e come complemento del lanciagranate XM307 Advanced Crew Served Weapon.
È in grado di essere convertita rapidamente in un XM307 con un piccolo numero di parti e pochi minuti di lavoro a livello di unità (e viceversa dall'XM307).
La legge sugli stanziamenti dell'esercizio 2008 ha assegnato $ 10 milioni alla General Dynamics per XM307 e XM312.
Nel maggio 2008 l' esercito americano aveva assegnato un contratto da 9 milioni di dollari al General Dynamics Armament and Technical Products (GDATP) per sviluppare una mitragliatrice leggera calibro .50 chiamata XM806 per integrare Browning M2. L'XM806 è stata annullata nel 2012. Attualmente l'esercito continuerà ad acquistare nuovi M2 Mk 19 per sostituire gli attuali mitragliatori che stanno esaurendo l’attività operativa di prima linea.
Specifiche:
Peso:
40 libbre (20 kg) max. (solo arma).
40 libbre (20 kg) max. (sistema di montaggio a terra).
Dimensioni: 9,9 W × 7,2 H × 61,5 L max. pollici (251 mm × 183 mm × 1562 mm) (52,5 L, 1334 mm) caricati).
Portabilità: portatile o montabile su di un veicolo.
Stabilità: altezza del treppiede fino a 18 pollici (460 mm).
Operazione: attualmente utilizza un gruppo operativo di gas ibrido e rinculo. Il gas alimenta il meccanismo dell’otturatore mentre il rinculo guida l'estensione della canna e il sistema di alimentazione. Sono in corso modifiche alla progettazione per eliminare totalmente il sistema a gas per offrire maggiore affidabilità e minore complessità.
Ambientale: operativamente insensibile alle condizioni meteo.
Sistema di alimentazione: bomboletta munita di armi o alimentabile da qualsiasi lattina usando l'attacco a campana. M9 link stripping posteriore — comune con munizioni M2 attuali. Alimentazione a sinistra, espulsione a destra di casi e collegamenti.
Stato del programma
Settembre 2005: l'XM312 venne testato dalle truppe della 1a divisione di fanteria nell'area di addestramento di Grafenwöhr in Germania.
ENGLISH
The XM312 is a heavy machine gun derived from the XM307 25 mm autocannon and chambered for the .50 BMG cartridge. It was designed in response to a request by the U.S. military for a replacement for the aging M2 Browning heavy machine gun, and as a complement to the heavier XM307 Advanced Crew Served Weapon grenade launcher.
It is capable of being converted quickly into an XM307 with a small number of parts and a few minutes of work at the unit level (and vice versa from the XM307).
The Fiscal Year 2008 Appropriations bill awarded $10 million to General Dynamics for the XM307 and XM312.
In May 2008 the U.S. Army had awarded General Dynamics Armament and Technical Products (GDATP) a $9 million contract to develop a lightweight .50-caliber machine gun called the XM806 to supplement the Browning M2. The XM806 was canceled in 2012. The Army at present will continue buying new M2s and Mk 19s to replenish the current guns that are wearing out.
Specifications
Weight:
40 pounds (20 kg) max. (weapon only).
40 pounds (20 kg) max. (ground mount system).
Dimensions: 9.9W × 7.2H × 61.5L max. inches (251 mm × 183 mm × 1562 mm) (52.5L, 1334 mm) charged).
Portability: Man portable or vehicle mountable.
Stability: Up to 18 inch (460 mm) tripod height.
Operation: Currently a hybrid gas & recoil operating group. Gas powers the bolt mechanism while recoil drives the barrel/barrel extension and the feed system. Design changes are underway to totally eliminate the gas system to provide increased reliability and reduced complexity.
Environmental: Operationally insensitive to conditions.
Feed system: Weapon-mountable ammunition can or feed from any can using bellmouth attachment. M9 rear stripping link—common with current M2 ammunition. Left hand feed, right hand eject of cases and links.
Program status
September 2005: The XM312 is test fired by troops from the 1st Infantry Division at the Grafenwöhr Training Area in Germany.
Lo Hughes AIM-4 Falcon fu il primo missile aria-aria operativo dell'United States Air Force.
Storia
Lo sviluppo di un missile guidato aria-aria iniziò nel 1946 quando la Hughes Aircraft vinse l'appalto per un missile subsonico il cui progetto era sotto il nome di MX-798, che portò al supersonico MX-904 nel 1947.
Il proposito originale di quest'arma si basava sull'autodifesa per gli aeroplani da bombardamento, ma dopo il 1950 si decise che invece sarebbe stato impiegato come arma principale nei caccia intercettori.
I primi collaudi iniziarono nel 1949 quando il progetto venne designato come AAM-A-2 o meglio battezzato come Falcon. Il Falcon fu anche denominato F-98 nel 1951, seguendo una moda passeggera di dare nomi simili a quelli degli aeroplani, ma nel 1955 fu nuovamente ribattezzato come GAR-1. I primi modelli di GAR-1 e GAR-2 entrarono in servizio nel 1956 a bordo del Northrop F-89 Scorpion, del McDonnell F-101B Voodoo e del Convair F-102 Delta Dagger. Furono prodotti circa 4 000 esemplari del GAR-1 ed in seguito venne rimpiazzato dal GAR-1D (denominato successivamente AIM-4A). Di questa variante furono prodotti circa 12 000 esemplari, il numero più grande del modello Falcon con SARH.
Il GAR-2 (chiamato poi AIM-4B) era un'arma a ricerca di calore e usava infrarossi anziché il SARH, ed aveva così il vantaggio di essere un'arma "fire and forget" ("spara e dimentica"), in quanto non era necessaria assistenza da parte dell'aereo che lo lanciava. Come accadeva nell'Unione Sovietica, era frequente l'uso di entrambi i tipi di arma, in modo da aumentare la possibilità di abbattere il nemico: l'arma a ricerca di calore veniva lanciata per prima, poi veniva un missile a guida radar. Venne poi il modello GAR-2A (noto anche come AIM-4C), il quale possedeva un modulo di ricerca di calore più efficiente. In totale furono prodotti 26 000 missili a ricerca di calore. Nel 1958 la Hughes introdusse una versione leggermente più grande del Falcon, denominata inizialmente GAR-3 Super Falcon, da cui venne estrapolato il successivo GAR-3A (AIM-4F) con un nuovo motore. L'equivalente del GAR-3, ma dotato di infrarossi, era denominato GAR-4A (AIM-4G). Furono prodotti circa 2 700 missili a guida radar e 3 400 a ricerca di calore.
La denominazione di AIM-4 giunse nel settembre 1963 dopo che furono create le versioni GAR-5 e GAR-6, i futuri AIM-26 Falcon. Una versione a lungo raggio fu creata per due aerei, l'XF-108 Rapier ed il Lockheed YF-12 con il codice GAR-9 (successivamente AIM-47 Falcon). Dati gli insuccessi conseguiti nella guerra del Vietnam, i progettisti della Huges crearono, nel 1970, un prototipo chiamato XAIM-4H dotato di un innesco di prossimità e di una carica esplosiva aumentata, ma non si raggiunse mai la produzione.
Impiego operativo
L'USAF iniziò ad usare quest'arma nella guerra del Vietnam sui caccia F-4D Phantom. Le sue performance in combattimento furono particolarmente scarse a causa degli alti tempi di raffreddamento del dispositivo di ricerca (dai 6 ai 7 secondi prima di diventare operativo), una riserva di refrigerante limitata che quando si esauriva rendeva inutilizzabile il missile, carica esplosiva insufficiente e mancanza di innesco con sensore di prossimità. Dopo questi insuccessi fu ritirato nel 1969 per essere rimpiazzato dal superiore AIM-9 Sidewinder.
Le varianti AIM-4F/4G Super Falcon rimasero in uso nell'USAF e nella Air National Guard, principalmente sugli F-102 Delta Dagger e sui F-106 Delta Dart fino a quando la serie completa fu ritirara nel 1988.
L'AIM-4C fu anche prodotto per le forze aeree svizzere con il nome in codice HM-58, e venne equipaggiato sui Mirage IIIS e dalle forze aeree svedesi nel Saab Draken e nel Saab Viggen.
Caratteristiche tecniche
Tutti i primi modelli di Falcon possedevano una piccola carica esplosiva (3,4 kg), la quale limitava il loro raggio letale. Un altro fattore limitante era l'assenza di un sensore di prossimità nell'innesco della carica: i sensori erano localizzati nelle ali e pertanto era necessario un colpo diretto per farlo detonare; inoltre i primi motori abbastanza potenti da permettere il lancio del Falcon da caccia supersonici vennero montati solamente nella versione F-98A, quindi si giunse, nella versione GAR-1, al motore Thiokol M58. Questa variante aveva un dispositivo di puntamento radar semi-attivo (SARH), il quale forniva un raggio operativo di circa 8 km. Il successivo GAR-1D aveva superfici di controllo più ampie e quindi una maggiore manovrabilità.
Il GAR-2 differiva invece dal GAR-1 per il sistema di guida ad infrarossi al posto del SARH, era circa 40 mm più lungo e 7 kg più pesante del modello a guida radar, mentre il raggio operativo era circa lo stesso. La successiva versione GAR-3 aveva un motore più potente (il Thiokol M46) che garantiva maggiore velocità e raggio operativo, una carica esplosiva più grande (13 kg). ed un sistema di guida migliore.
Nel GAR-2B il telaio era derivato dalle prime versioni del GAR-1/GAR-2 ed il modulo a ricerca di calore era una versione migliorata di quelli installati nel GAR-4A.
ENGLISH
The Hughes AIM-4 Falcon was the first operational guided air-to-air missile of the United States Air Force. Development began in 1946; the weapon was first tested in 1949. The missile entered service with the USAF in 1956.
Produced in both heat-seeking and radar-guided versions, the missile served during the Vietnam War with USAF McDonnell Douglas F-4 Phantom II units. Designed to shoot down slow bombers with limited maneuverability, it was ineffective against maneuverable fighters over Vietnam. Lacking proximity fusing, the missile would only detonate if a direct hit was scored. Only five kills were recorded.
With the AIM-4's poor kill record rendering the F-4 ineffective at air-to-air combat, the fighters were modified to carry the USN-designed AIM-9 Sidewinder missile instead, which was already carried on USN and USMC F-4 Phantom II and F-8 Crusader jet fighters. The Sidewinder was much more effective and continues to serve the armed forces of the United States and numerous allied nations to this day.
Development
Defensive concept
Development of a guided air-to-air missile began in 1946. Hughes Aircraft was awarded a contract for a subsonic missile under the project designation MX-798, which soon gave way to the supersonic MX-904 in 1947.
The original purpose of the weapon was as a self-defense weapon for bomber aircraft, which would carry a magazine of three missiles in the rear fuselage, and fire them through a long tube that led through the area that normally held the tail turret. In the case of the B-52, the missile contained a tuner for the bomber's A-3 rear-facing radar, and would follow the signal being reflected off the target aircraft using a semi-active radar homing (SARH) system.
Anti-bomber development
At the same time that the original MX-798 had been released, a specification for a forward-firing missile for fighter aircraft had been released as MX-799. This had progressed to the point of testing prototype rounds, as the AAM-A-1 Firebird, when its subsonic speed and manual guidance were realized to be serious problems.
The project was cancelled, and the recently released MX-904 was redirected to replace Firebird in the anti-bomber role. At this stage the weapon was still designed to be fired out of a tube, now leading from a weapon bay behind the nose-mounted radar with the launch tube exiting below the radar antenna. Instead of a magazine with multiple missiles, three missiles were placed in the tube tip-to-tail.
Housing in a tube presented several problems, but primary among them was that there was no way for the missile's seeker to lock-on before launch. The original concept would be firing against interceptor aircraft that were slowly approaching the B-52 and would be somewhere fairly close to directly behind the aircraft. In the case of a fighter, the target might not be so conveniently located, and with no way to know if it could see the target while inside the tube, this meant it might never lock-on properly.
Eventually, it was decided to abandon the tube-launched concept and mount the missile on the wings or in weapon bays that would point the missile at the target prior to launch. This change also allowed the seeker to use infrared homing as well as SARH. Interchangeable seekers were developed, allowing an aircraft to carry either type, or both. Additionally, freed from the tube, the missile's wings were allowed to grow larger and took on the long delta form that it and its various descendants would carry into the 2000s.
Testing and service
The first test firings took place in 1949, at which time it was designated AAM-A-2 and given the popular name Falcon. A brief policy of assigning fighter and bomber designations to missiles led it to be redesignated F-98 in 1951. In 1955, the policy changed again, and the missile was again redesignated GAR-1.
The initial GAR-1 and GAR-2 models entered service in 1956. It armed the Northrop F-89 Scorpion, McDonnell F-101B Voodoo and Convair F-102 Delta Dagger and F-106 Delta Dart interceptors. The only other users were Canada, Finland, Sweden and Switzerland, whose CF-101 Voodoo, Saab 35 Draken and Dassault Mirage IIIS carried the Falcon. Canada also hoped to use them on the Avro Canada CF-105 Arrow interceptor; however, this was never realized because of the Arrow's cancellation.
Fighters carrying the Falcon were often designed with internal weapons bays for carrying this missile. The Scorpion carried them on wingtip pods, while the Delta Dagger and Delta Dart had belly bays with a trapeze mechanism to move them into the airstream for launch. The F-101B had an unusual bay arrangement where two were stored externally, and then the bay door would rotate to expose two more missiles. It is likely the General Dynamics F-111's internal bay would have accommodated the missile as well, but by the time of service the Air Force had already dropped the Falcon for use against fighters, as well as the idea of using the F-111 as an air combat fighter.
The GAR-1 had semi-active radar homing (SARH), giving a range of about 5 mi (8.0 km). About 4,000 missiles were produced. It was replaced in production by the GAR-1D (later AIM-4A), with larger control surfaces. About 12,000 of this variant were produced, the major production version of the SARH Falcon.
The GAR-2 (later AIM-4B) was a heat-seeker, generally limited to rear-aspect engagements, but with the advantage of being a 'fire and forget' weapon. As would also be Soviet practice, it was common to fire the weapon in salvos of both types to increase the chances of a hit (a heat-seeking missile fired first, followed moments later by a radar-guided missile). The GAR-2 was about 1.5 in (40 mm) longer and 16 lb (7 kg) heavier than its SARH counterpart. Its range was similar. It was replaced in production by the GAR-2A (later AIM-4C), with a more sensitive infrared seeker. A total of about 26,000 of the infrared-homing Falcons were built.
All of the early Falcons had a small 7.6 lb (3.4 kg) warhead, limiting their lethal radius. Also limiting them tactically was the fact that Falcon lacked a proximity fuze: the fuzing for the missile was in the leading edges of the wings, requiring a direct hit to detonate.
In 1958, Hughes introduced a slightly enlarged version of the Falcon, initially dubbed Super Falcon, with a more powerful, longer-burning rocket engine, increasing speed and range. It had a larger warhead (28.7 lb / 13 kg) and better guidance systems. The SARH versions were GAR-3 (AIM-4E) and the improved GAR-3A (AIM-4F). The infrared version was the GAR-4A (AIM-4G). About 2,700 SARH missiles and 3,400 IR Super Falcons were produced, replacing most earlier versions of the weapon in service.
The Falcon was redesignated AIM-4 in September 1962.
The final version of the original Falcon was the GAR-2B (later AIM-4D), which entered service in 1963. This was intended as a fighter combat weapon, combining the lighter, smaller airframe of the earlier GAR-1/GAR-2 weapon with the improved IR seeker of the GAR-4A/AIM-4G.
An effort to address the limitations of AIM-4D led to the development in 1970 of the XAIM-4H, which had a laser proximity fuze, new warhead, and better maneuverability. It was cancelled the following year without entering service.
A larger version of the Falcon carrying a 0.25-kiloton nuclear warhead was developed as the GAR-11 (later designated the AIM-26 Falcon), while a long-range version was developed for the North American XF-108 Rapier and Lockheed YF-12 interceptors as the GAR-9 (later AIM-47 Falcon).
Operational history
The Air Force deployed AIM-4 in May 1967 during the Vietnam War on the new F-4D Phantom II, which carried it on the inner wing pylons and was not wired to carry the AIM-9 Sidewinder. The missile's combat performance was very poor. The Falcon, already operational on Air Defense Command aircraft, was designed to be used against bombers, and its slow seeker cooling times (as much as six or seven seconds to obtain a lock on a target) rendered it largely ineffective against maneuvering fighters. Moreover, it could only be cooled once. Limited coolant supply meant that once cooled, the missile would expend its supply of liquid nitrogen in two minutes, rendering it useless on the rail. The missile also had a small warhead, and lacked proximity fusing. As a result, only five kills were scored, all with the AIM-4D version. (The Falcon was also experimentally fired by the F-102 Delta Dagger against ground targets at night using its infrared seeker.)
The weapon was unpopular with pilots from the onset and was supplemented or partially withdrawn in 1969, to be replaced in the F-4D by the Sidewinder after retrofitting the proper wiring. Colonel Robin Olds, USAF, commanding the F-4D-equipped 8th Tactical Fighter Wing, was an outspoken critic of the missile and said of it:
By the beginning of June, we all hated the new AIM-4 Falcon missiles. I loathed the damned useless things. I wanted my Sidewinders back. In two missions I had fired seven or eight of the bloody things and not one guided. They were worse than I had anticipated. Sometimes they refused to launch; sometimes they just cruised off into the blue without guiding. In the thick of an engagement with my head twisting and turning, trying to keep track of friend and foe, I'd forget which of the four I had (already) selected and couldn't tell which of the remaining was perking and which head was already expiring on its launch rail. Twice upon returning to base I had the tech rep go over the switchology and firing sequences. We never discovered I was doing anything wrong.
Colonel Olds became exasperated with the Falcon's poor combat performance. He ordered his entire fighter wing to rewire the F-4Ds to carry more reliable AIM-9 Sidewinders. Although it was an unauthorized field modification, the entire air force eventually followed his example.
Vietnam War: U.S. AIM-4 Falcon Air to Air Victories
Used from 1965 through 1972 in Vietnam, Falcons achieved their only kills during Operation Rolling Thunder (1965–68) during which time only 5 successful hits were scored from 54 launchings during aerial combat.
The AIM-4C was also produced as the HM-58 for the Swiss Air Force for use on the Dassault Mirage IIIS, and license-manufactured in Sweden for the Swedish Air Force (as the Rb 28) to equip the Saab 35 Draken and 37 Viggen. The seeker of the missile was also re-designed.
The AIM-4F/AIM-4G Super Falcon remained in USAF and ANG service, primarily with Convair F-102 Delta Dagger and F-106 Delta Dart interceptors, until the final retirement of the F-106 in 1988. These aircraft had been designed to carry the weapon and could not be easily converted to carry larger weapons like the Sidewinder or AIM-7 Sparrow, which were much longer.
