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[Rythena] X-32 AGM Loadout

The Boeing X-32 is a concept demonstrator aircraft that was designed for the Joint Strike Fighter competition. It lost to the Lockheed Martin X-35 demonstrator, which was further developed into the Lockheed Martin F-35 Lightning II.

Boeing's strategy for a competitive advantage was to offer substantially lower manufacturing and life-cycle costs by minimizing variations between the different JSF versions. The X-32 therefore was designed around a large one piece carbon fiber composite delta wing. The wing had a span of 9.15 meters, with a 55-degree leading edge sweep, and could hold up to 20,000 pounds (9,000 kg) of fuel. The purpose of the high sweep angle was to allow for a thick wing section to be used while still providing limited transonic aerodynamic drag, and to provide a good angle for wing-installed conformal antenna equipment. The wing would prove a challenge to fabricate.

The compete-on-cost strategy also led Boeing to pick a direct-lift thrust vectoring system, for the Marines' short take-off and vertical landing (STOVL) requirement, as this would only necessitate the addition of a thrust vectoring module around the main engine. However, this choice required the engine to be mounted directly behind the cockpit, and moved the center of gravity forward from its usual position in jet fighters (towards the rear of the airplane) to enable a neutral-attitude hover. Boeing had proposed, in the 1960s, a similar supersonic fighter with a mid-center-of-gravity mounted engine with vectored thrust nozzles, but this never proceeded beyond pictures published in Aviation Week.[citation needed] By comparison, the Lockheed entry looked like, if anything, a smaller version of the F-22 Raptor stealth fighter. Yet another effect of the selection of the direct-lift system was the large chin-mounted air intake. This was required to feed sufficient air to the main engine (to provide the thrust necessary to hover) during the zero horizontal velocity phase, when it could not exploit ram-air pressure. A knock-on effect of this large intake was the potential direct visibility of the compressor blades to radar (see radar cross-section). Mitigation possibilities included variable baffles designed to block incoming radio waves without adversely affecting airflow.

Wikipedia Stuff

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Speed- 510 kph
Range - 110km
Powerhouse- Pratt & Whitney YF119-PW-614
8 Hardpoints
Laser Designation
High Realism
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Armament-
Single 30mm Autocannon
6 Aim-230 Excalibur BVRAMM
2 Aim-99 Diamondback
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Startup-
1. Get in seat
2. Press 1
3. Press 2
4. Flip everything on the Left inner Conole (Exept fuel pumps)
5. Engine Control System (ECS)
6.Fuel pumps
7. Check Fuel
8. Flip remaining switches on left consoul
9. Lamp/NG1 on
10. Throttle 0.3
11. VSTOL on
12.Hold starter
13. Confirm engine RPS stability, do not attempt flight if super erratic.
14. MFD modes on
15. Liftoff confirm in open area
16. Your flying in VTOL now
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Standard Flight proceadure-
Flip VSTOL to off
Confirm forward speed increase
Climb to 250 alt (Reccomended)
Set Turbofan to 0.8 and throttle to 0.6
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Credits-
https://steamproxy.net/sharedfiles/filedetails/?id=1799889445 Map
https://steamproxy.net/sharedfiles/filedetails/?id=2793872276 MFDs
https://steamproxy.net/sharedfiles/filedetails/?id=2819788897 HUD
https://steamproxy.net/sharedfiles/filedetails/?id=2648490664 Weapons screen
https://steamproxy.net/sharedfiles/filedetails/?id=2037028237 CSM
https://steamproxy.net/sharedfiles/filedetails/?id=2831866315 Radar
https://steamproxy.net/sharedfiles/filedetails/?id=2049324674 Fuel thingy
https://steamproxy.net/sharedfiles/filedetails/?id=2277818149 Transponder\

Used the Newquay L-02 Republique for 2 of the pictures.

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Riverala- Cockpit Detail, Cockpit Operations, Quality Check
Cailean.Coleman - Main body, Microcontrolers, FLCS, Weapons, Engine.

DO NOT REUPLOAD!
Ignore my vilolent button mashing in the startup vid XD


This is partly AGM, but is mainly uploaded for the FLIR based X-32 release.