Aaz>> что ж ты ТТЗ не хочешь прочитать? tramp_> рад бы, однако нет возможности.
Придется тебе ее дать (хотя простыня получится). Итак, "слушайте, и не говорите, что не слышали". (с)
Преамбулу пропускаю - там "воды" слишком много.
LAAR AIRCRAFT REQUIREMENTS
A. Critical Requirements: Fixed-wing aircraft must meet all of the requirements listed below:
1. Properly certified for day/night visual flight rules/instrument flight rules (VFR/IFR) operations.
2. Properly certified to meet acquisition requirements and allow for U.S. Military operation. Systems/capability must meet U.S. government releasability / exportability requirements.
3. Aircraft must support a 450 flight hours per platform, per year, operations tempo with an aircraft availability rate of ninety percent (90%) Mission Capable (MC) for completion of day and night missions under Visual Meteorological Conditions (VMC). Platforms must be capable of sustaining an eighty percent (80%) Fully Mission Capable (FMC) rate for the completion of missions under Instrument Meteorological Conditions (IMC), in the environmental conditions expected in Partner Nations (PN) Theatre of Operations (i.e. up to 50-degrees Celsius).
4. Capable of conducting operations from semi-prepared surfaces (dirt, grass, gravel, etc.).
5. Capable of operating from an austere, forward operating base without any ground support other than fuel being available for re-fueling operations.
6. Powerplant(s) capable of burning JP-8 or Jet-A fuel.
7. Dual, tandem seat with dual controls to facilitate dual use as light attack/armed reconnaissance as well as an advanced trainer. Configuration should be similar to allow full control, to include conducting instrument approaches and landings, from either cockpit for both pilots.
8. Zero altitude-zero airspeed ejection seats.
9. Common multi-function display (MFD) cockpit configuration for all aircraft to include Wide Area Augmentation System (WAAS) and Vertical Navigation-certified Global Positioning System (GPS) navigation capability to allow day/night, all-weather instrument flight, especially into airfields which do not possess navigational aids.
10. Flight visibility: Aircraft must allow a full 270 horizontal degree field of view from the front cockpit field centered on the nose of the aircraft. Minimal obstructions permitted, i.e. window frames, canopy rails, low wing, heads-up display (HUD).
11. Front cockpit must have a HUD with an air-to-ground system capable of computing and displaying the continuously computed impact point (CCIP), continuously computed release point (CCRP), strafe, and manual weapon aiming computation/release.
12. Must have a defensive measures package to include a radar warning receiver (RWR), missile approach warning system (MAWS), and chaff and flare dispensers.
13. Armored cockpits and engine compartment to protect from small arms fire. Self-sealing fuel tanks required.
14. Night Vision Goggle (NVG) compatible cockpits, including lighting and instrumentation.
15. Air conditioning system capable of cooling the aircraft cockpit and avionics within operational limits for outside temperatures up to 50 degrees Celsius to include solar gain.
16. On-board oxygen generating system (OBOGS).
17. Flight duration: Aircraft, equipped with external fuel tanks and a common design payload, must fly 5.0 hour sorties plus 30 minutes fuel reserves. Aircraft must have a 900 nautical mile (NM) self-deployment ferry range.
18. Avionics: IFR capable. Dual Comm with single Nav/ Hobbs meter/ Mode C reporting transponder, Global Positioning System (GPS), audio panel and integral intercom meeting US Military Standard (Mil Std) (compatible with USAF-standard headsets and/or helmets). Must be Instrument Landing System (ILS), Very High Frequency (VHF) Omnidirectional Range (VOR)/Distance Measuring Equipment (DME), and/or GPS approach compatible.
19. Communications suite shall consist of internal crew intercom and the ability to communicate to Air Traffic Control (ATC) facilities and operational agencies, both line of sight (LOS) and beyond line of sight (BLOS) via voice on: Civil/ Military VHF Voice, Military Ultra High Frequency (UHF) and Voice Civil UHF. Able to transmit/receive simultaneously on three (3) radios. The voice communications system shall have the capability to be upgraded to accommodate secure voice communications.
20. Accommodate pilots 64–77 inches tall and sitting heights of 34–40 inches.
21. Aircraft flight controls: All aircraft flight and fuel controls, and critical/essential circuit breakers must be accessible from front cockpit, with seat belts/shoulder harnesses fastened.
22. Instrumentation: All aircraft controls and instruments within each cockpit must be visible and accessible from the seat, with seat belts/shoulder harnesses fastened.
23. Data link ability to provide future capability (LOS required, BLOS desired). Transmit and receive real-time, full-motion video and still imagery. Video downlink capability compatible with Remote Operations Video Enhanced Receiver (ROVER). Variable message format (VMF) digital communications capability compatible with the ground forward air control / joint terminal attack control (FAC/JTAC) systems
24. Intelligence, Surveillance and Reconnaissance (ISR) subsystems
a. The desired ISR sensor suite should be capable of providing electro-optical and infrared full motion video and photographs.
b. Capable of laser designation, laser marking, laser spot tracking, and self-derivation of accurate coordinates.
c. Capable of allowing post flight download data link as described above.
25. The aircraft must be capable of employing a variety of air-to-ground weapons and munitions, up to an employment altitude of 10,000 feet AGL, including aerial gunnery, unguided free-fall munitions, precision munitions and battlefield illumination devices. The aircraft must have override capability to disable weapons delivery authority from either cockpit. The aircraft must be capable, but not limited, to the following:
a. At least four weapons stations, two of which may be used for external fuel.
b. Carry a minimum of two 500-pound class munitions
c. Must have a laser designator to employ laser-guided weapons.
d. Must have the capability to generate coordinates with onboard sensors
e. Capability to employ aerial gunnery
f. Capability to employ 2.75 inch rockets
g. Capability to employ rail launched munitions
h. Capability to employ overt and covert air-dropped flares (illumination rounds)
i. Weapons interface databus to integrate current applicable weapons United States DoD inventory
B. Aircraft desired requirements
1. Infrared (IR) suppression for engine(s)
2. Anti-ice/de-ice system to allow flight in moderate icing conditions
3. Sufficient dust and sand filters to be capable of conducting desert environment operations
4. Aircraft is to have a 30,000 feet operational altitude.
5. Takeoff within 6000 feet of available runway and meet a 200 ft/nm climb gradient at pressure altitudes up to 6000 feet and temperatures up to 40 degrees Celsius with a common design payload at a typical mission weight.
6. Land within 6000 feet of available runway at pressure altitudes up to 6000’ feet and temperatures up to 40 degrees Celsius with a common design payload and the maximum landing weight for the aircraft.
7. Continuous cruise speed: 180 Knots True Air Speed (KTAS) (minimum) at 10,000 feet density altitude on a standard day and full fuel minus that fuel required to taxi out, take off, and climb to 10,000 feet above ground level (AGL) from sea level with a common design payload and configuration.
8. Aerobatic capable of performing the following maneuvers with clean configuration (no stores): aileron roll, barrel roll, chandelle, cloverleaf, Cuban eight, Immelman turn, lazy eight, loop, and split-S.
9. To allow for a shorter logistics trail, all aircraft should be configured to be readily available for use as either a two-seat advanced trainer or a two-seat attack/armed reconnaissance platform with no field level conversion necessary other than loading munitions or stores (see item number A.25 above for munitions/stores).
Aaz> Есть режимы СУО для задач "в-п" tramp_> Это ведь не отрицает приоритет высокоточного оружия?
И кем этот приоритет установлен - некоторыми участниками форума А-Базы?
Во всяком случае, в ТТЗ (как ты теперь можешь убедиться), об этом приоритете ничего не говорится.
Aaz> Кстати, слова о том, что CCIP и CCRP есть, якобы, какие-то "особо точные методы прицеливания" tramp_> стоп-стоп, программа модернизации Су-24 Гефест это что, перелицовка старых методов?
Естественно.
Вообще говоря, CCIP и CCRP есть
способы представления летчику информации, необходимой для применения оружия. В первом случае на ИЛС постоянно выводится точка, в которую попадет бомба / НУРС / очередь из пушки (в зависимости от положения переключателя "выбор оружия"), если "вот сейчас" нажать на гашетку.
Второй метод заключается в том, что при атаке заранее выбранной (вводом координат, наложением марки прицела или марки лазерного дальномера) цели на ИЛС выводятся "подсказки", куда надо доворачивать, чтобы поразить эту цель. В момент, когда нужно применять оружие, на ИЛС появляется надпись "Сброс/Пуск" (может задействоваться также речевой информатор).
Как видишь, к точности применения оружия это не имеет никакого отношения. Да, можно повысить возможности вычислителя, установить новые СВС и ИНС, улучшить алгоритмы вычисления - но сути методов CCIP и CCRP это не меняет.
Aaz>> strafe - это режим штурмовки / атаки с малой высоты. Aaz>> Что такое manual, думаю, объяснять не надо... tramp_> если так выдтрать с мясом цитаты, то доказать можно что угодно.
Теперь ты можешь убедиться, что никакого выдирания нет - я перечислил
ВСЕ режимы работы ИЛС/СУВ, заданные в ТТЗ.
tramp_> Хорошо, дабы не не попасть в клинику им.36 тысяч Ил-2 изменю формулировку на "преимущественно/предпочтительно управляемое/высокоточное оружие"
ОК, при такой формулировке тебе не надо в стационар - можно ограничиться амбулаторным лечением.