Paradisius
10-11-2004, 04:23
The small Socialist nation of Paradisius is on a search to purchase weapons geared towards defense, but in extreme cases could be used in military strikes.
We would also like to ask for liberal socialist nations to move into negotiations so that we can spread the greatness of socialism.
Hamanistan
10-11-2004, 04:28
Modern weapons that are being sold cheap from Hamanistan Industries:
20 T-92 Tank's at $900 each.
10 SAM Site launchers and missiles at $5,000
50 SAM Missiles for $1000
50 AT 5th Generation Anti-Tank Rocket Launchers at $100 each.
Tannelorn
10-11-2004, 04:35
Incredibly high quality future tech weapons and equipment for sale at reasonable prices, or blanket deals, cut rates for authoritarian governments
we offer anything from star ships to mobile frames, to guns and armour, artillery and nuclear weapons also for sale or lease.
Remember At tannelorn its the consumer first, there enemies second
The Macabees
10-11-2004, 04:35
This crap is rather expensive...and it's just for you - because I feel like making money - but it's worth it! You can't produce them..or sell them though!
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Panzerkampfwaggen IX Sargon Ausf. B -
The armor is composed of a diamond helix bonded through double carbon bonds and other ADBOND designs around and through a buckyball matrix, layered in 240 nano-meter strips. This is covered by the Indium/Osmium-Germanium mix 2nd Gen Supercooled Coil, which was stolen off an Iscariot VIII a while back. They are filled with supercooled liquid Xenon and when a round impacts, the liquid gasses out to counter the heat while the metal coil itself is used as a heat conductor to dissipate the attack it will render that portion of the coil useless but should still enable it to work on other parts of the tank. Especially good against HEAT. Finally there is a thick layer of NxRA Ablative Armor Blocks, up to 14cm in some places. This provides up to an additional 1000mm RHA, for a total of up to 4500mm RHA. (max. real thickness 200mm). However, the central differences between the Spanish buckyball matrix and the composites of the armor is the type of bondage between the diamond helix, allowing for a stronger chemical bonding, meaning the armor RHA will be a tad stronger.
The engine of the Variant B of the Sargon tank is a 2,000 horsepower diesel engine, hitting a maximum velocity of 40 kilometers per hour. However, the diesel conserves more fuel than a conventional gasoline engine. The Sargon will rarely cruise past thirty however, due to the fact that most of the world’s roads don’t have the strength to deal with a huge beast, such as the Sargon, at 40 kph. The engine if furthermore enhanced with ceramic composite parts giving the engine a brutal strength of 5,000 horsepower, need be. However, again, rarely will so much raw power be used. The engine is cooled by a xenon fuel tank, and a super condensing cooling gel which spreads over the ceramic compositing.
The Variant B Sargon has a 150mm L/70 ETC gun. The L/70 length gives it the power of up to a 200mm gun, with a lower muzzle flash, and an extremely low recoil. Furthermore, “R” rings, composed of small springs measuring mere nano-meters, composed of a nylon crystal composite, lower the recoil allowing the tank to recover in between rounds much faster. Consequently, the reloading and firing process lowers considerably, allowing more rounds to be popped out. The fire and control allows the gunner to process and lock onto up to twenty different targets all at once. The main gun also has a Thermal Layer to allow the gun to cool down after each round.
For missile defense the Ausf. B is given two ADMS-1 guns, capable of locking on, through on board RADAR and LIDAR detection, incoming anti-tank rounds and other general missiles. The ADMS-1 then fires a batch of RRS bullets and blows the incoming missile pre-emptively. This is similar to the workings of MetalStorm, however, is much smaller, and has a lesser chance of being blown off the tank by a stray bullet during close combat exercises.
The commander has a full 360 degree view, provided by three cameras on the tank, giving the commander views of the battlefield on three separate LCD screens in his small compartment. This allows for the commander to have an enhanced view of the targets available and decreases chances of ambushes.
COST: 110 Million
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MTAAM-2 Predator Air to Air Missile
After facing the Romanian air to air missile the Spaniards began working on their own air to air missiles that could match and exceed the Romanian (South African) missiles. The work concluded with the MTAAM-2 Predator.
The Predator turbojet engine is made up a single crystal NiFe based superallow, called THYMONEL 8. THYMONEL 8 has a high fatigue resistance and this teams up with a low hydrogen enviroment embrittlement (HEE). Furthermore, THYMONEL 8 exihibits higher termal conductivity and lower Young's modulus than the single crystals used for turbine engines, consequently beneficial for the thermo-mechanical strength. (OOC: Not techno-babble... I researched this out of a three thousand page book on super allows - took me about two weeks to read the necessary sections.)
The single crystal superallow is termed third generation and is better known as Rene N6. Rene N6 is microstructurally stable and is about thirty degrees stronger than its second generation counterpart. SRZ, a cellual precipitation reaction that primarily occurs beneath coatins, was countred by the improved Rene N6.
The turbojet engine incorporates the scramjet phenomenon, which was designed in the early 80s to allow missiles to cover large tracks of displacement. In a thick atmosphere enviroment (sea-skimmers) scramjet cannot work, but for an air to air missile scramjet is prime. The more delictate scramjet propulsion used in the MTAAM-2 pushes the missiles to Mach 4.7 in altitudes ten thousand feet or above, and up to Mach 8 in the upper atmosphere, were air friction is not a problem, making the MTAAM-2 also a great sattelite killer. The Predator, working with scramjet and a much thinner body to decrease the impression of air friction has a maximum range of 200 kilometers (ca. 180 miles).
The missile has a 20kg warhead. It doesn't take much to shoot an aircraft out of the sky. The Octogen warhead is a high explosive, meaning if the missile explodes within ten feet it will still cause massive damage on the aircraft, or in most cases down it.
The MTAAM-2 uses MRT-3 (dropped the TENEX SPY-6) RADAR technology to track its targets, as well as MLT-1 LIDAR Technology. The LRT-1 has both Doppler LIDAR which measures the velocity of the target by using the wavelength of the light reflectet or scattered by the target, and range finder LIDAR. LIDAR is insensitive to chaff or IR flares.
COST: 2 million
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MMA-A2 Hawk
Maximum Speed: Mach 3.4
Supercruise: Mach 2.1
WingSpan: 36 feet
Internal Fuel: 16,000 lbs
Payload: 1,000 lbs
Take-off weight is 20 tonnes
2 MVL V1 Thrust Engines
Armament:
1 30mm Vulcan
18 A-11 Archers
2 500lb cruise missiles
The Aircrafts 8 Internal Hardpoints can carry Air-To-Surface Missiles,Air-to-Air Missiles,Bombs and also ECM Pods for electronic warfare.
RADAR:
The Hawk uses a miniature, but upgraded, TENEX Spy-6 RADAR system, which burns through all known stealth equipment at 76 kilometers. The land based Spy- has a range of 670kms. "It utilises the steerable radar beam first developed for the SPY-5 system, meaning that aircraft or missiles linked to this system can have their own internal radars off and still have an electronic contact better than if they were standalone." (Iraq)
Max Ceiling:
Some 70,000 feet.
Life Support Systems.
The Hawk life support system integrates all critical components of clothing, protective gear, and aircraft equipment necessary to sustain the pilot's life while flying the aircraft. In the past, these components had been designed and produced separately. The life support system components include:
An on-board oxygen generation system that supplies breathable air to the pilot.
An integrated breathing regulator/anti-g valve (BRAG) that controls flow and pressure to the mask and pressure garments.
A chemical/biological/cold-water immersion protection ensemble.
An upper body counterpressure garment and a lower body anti-G garment acts a partial pressure suit at high altitudes.
An air-cooling garment thermal relief for the pilot.
Helmet and helmet-mounted systems including C/B goggles and C/B hood; and the a breathing mask and hose system
The Hawk uses liquid cooling, rather than air cooling for the mission avionics. Su-48 is breaking ground in liquid cooling and the environment in which it works. Resistance to high temperature and durability were the driving factors in the liquid cooling design.
There are six fuel tanks on the Hawk, including one in the forward fuselage behind the pilot's ejection seat. The others are located in the fuselage and the wings.
The Hawk Communications/Navigation/Identification (CNI) 'system' is a collection of communication, navigation, and identification functions, once again employing the CIP for signal and data processing resources. Each CNI function has its associated aperture installed throughout the aircraft.
Included in the Communications/Navigation/Identification (CNI) system is an Inter/Intra-Flight Data Link (IFDL) that allows all Hawk in a flight to share target and system data automatically and without radio calls. The Inter/Intra Flight Data Link is one of the powerful tools that make all Hawk more capable. One of the original objectives for the Su-48 was to increase the percentage of fighter pilots who make 'kills'. With the IFDL, each pilot is free to operate more autonomously because, for example, the leader can tell at a glance what his wing man's fuel state is, his weapons remaining, and even the enemy aircraft he has targeted. Targets can be automatically prioritized and set up in a shoot list with one button push. A 'shoot' cue in the head up display alerts the pilot to the selected weapon kill parameters and he fires the weapons. Both a pilot's and wing man's missile flight can be monitored on the cockpit displays. Classical tactics based on visual 'tally' (visual identification) and violent formation maneuvers that reduce the wing man to 'hanging on' may have to be rethought in light of such capabilities. This link also allows additional Su-48 flights to be added to the net for multi-flight coordinated attack.
The Electronic Warfare 'system' is also a collection of apertures, electronics, and processors (again using the CIP) that detect and locate signals from other aircraft and controls the Hawk expendable countermeasures (chaff and flares). The EW aperture locations provide all-aspect coverage, and the system includes a missile launch detection capability.
The Hawks electronic warfare system includes a radar warning receiver and a missile launch detector.
The Stores Management System (SMS) controls weapons launch sequences, including door control (for the internal weapons carriage) and emergency weapons jettison.
The power supply modules designed for the Hawk avionics are cooled with polyalphaolefin (PAO) liquid coolant to carry away heat generated by the supplies' power-conversion process. The reduced temperature allows the component's power output to increase from 250 watts to 400 watts. Each module measure 6.41 inches by 5.99 inches by 0.58 inches and weighs 1.8 pounds.
The avionics racks, located in the forward fuselage, contain the processing, not only for the mission avionics, but also for the Vehicle Management System (VMS) and Integrated Vehicle System Controller (IVSC). The flight worthy racks, including the liquid-flowthrough racks required for the CIP.
Two Litton LN-100F ring laser gyroscopes in the forward fuselage provide the aircraft a self-contained method of knowing where it is. These inertial measurement units, placed nose to nose behind the radar on the aircraft's centerline, are operated off separate data buses to provide independent measurement data. In normal flight, IRS data is fused with Global Positioning System (GPS) data to provide an extremely reliable navigational capability. The IMUs are the only completely reliable source of data for the aircraft at attitudes above 30 degrees angle of attack (AOA). One of the IRS units feeds data directly into the CIP for gun control steering.
The Flying Test Bed (FTB) represents an interim test environment between the controlled, but static environment of the ground labs, and the dynamic flight testing of the Hawk. Sensor systems installed in the aircraft, CIPs, as well as operator consoles and instrumentation will be used to test avionics capabilities prior to release to the Hawk.
Building Cost: 350 million (very expensive factory equipment)
COST: 90 million USD
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Panzerwerfer Ausf. B
The highly effective Panzerwerfer MLRS is designed to suppress missile, artillery and mortar batteries, destroy strong points and eliminate enemy strongholds, as well as to defeat enemy's manpower, armoured and unarmoured materiel and other targets at the operational level. The system is highly mobile and transportable even off-roads. It can be used in different climatic conditions at an ambient temperature ranging from +50oC to -50oC.
The Panzerwerfer Combat Vehicle comprises a 30-tube launcher system mounted on an automobile chassis (8 x 8) of high cross-country ability with a powerful diesel engine. The single SMERCH unit is capable of firing a complete 20-round salvo within 20 seconds engaging an area of 672000 sq.m. High accuracy of fire with salvo dispersion is provided by in-flight rotation technique of a rocket projectile specially designed for this MLRS. Fire can be controlled from the special cabin of the combat vehicle or remotely.
The rocket used is the 300 mm calibre 9M55K (Russian), fitted with a self-contained powered-flight phase control system enhancing fire precision by a factor of two and accuracy by a factor of three as compared to unguided rockets. Minimum range is 20,000 m and maximum range 70,000 m.
The rocket can be fitted with the following types of warheads:
9M55K cluster projectile with fragmentation sub-munitions (72 x 1.81 kg). Intended to engage manpower, soft material;
9M55F with a separable HE warhead containing 95 kg of explosive for use against lightly armoured vehicles, fortifications and personnel;
9M55K1 with five top-attack anti-armour sub-munitions that weigh 15 kg each and are fitted with a two-band infra-red seeker. The munition measures 284x255x186 mm, the seeker's field of view is 30 deg. designed to defeat armour.
9M55S 300 mm rocket projectile with a thermobaric warhead is designed to defeat unsheltered manpower, as well as personel in light field fortifications and in soft-skinned/lightly armored vehichles. The warhead weght is 243 kg, the weight of explosive is 100 kg, the diameter of the thermobaric field with the temperature more than 1000 °C is 25 m.
9M55K4 300 mm rocket projectile is designed for remote laying of anti-tank minefields. The number of mines is 25. The mine weighs 4.85kg, the weight of explosive is 1.85 kg. Time of mine self-destruction is 16 ... 24 hours.
COST: 20 Million (50,000 per rocket not included)
Paradisius
10-11-2004, 04:59
To the Macabree nation. The USSP is wiring you most of our entire military funds to purchase:
MTAAM-2 (1)
MMA-A2 (2)
The funds were mainly from the corporations we took control over when we convereted to an extremely Socialist government. We would like to thank your nation, and hope that you will convert to a more liberal and socialist standing in the future. However, it is never our place to judge other people's beliefs.