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Added mucho stuff again #39

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81 changes: 78 additions & 3 deletions src/cockpit/pilot/left_console/front_section.md
Original file line number Diff line number Diff line change
Expand Up @@ -100,7 +100,7 @@ Used to select the appropriate contrast conditions for seeker acquisition with
the AGM-65A and B.

| Name | Description |
| ------- | ------------------------------------------------------------------------- |
|---------|---------------------------------------------------------------------------|
| WHT/BLK | Programs the missile seeker to track a light target on a dark background. |
| AUTO | Programs the missile to use its automatic tracking mode. |
| BLK/WHT | Programs the missile seeker to track a dark target on a light background. |
Expand All @@ -117,7 +117,7 @@ disengage the Static Pressure Compensation of the altimeter, thus eliminating,
or invoking, altimeter lag from rapid altitude changes.

| Name | Description |
| ---------- | ------------------------------------------------------------------------------------------------- |
|------------|---------------------------------------------------------------------------------------------------|
| RESET CORR | Actuated after engine startup, then in flight if a SPC warning is caused by transient conditions. |
| NORM | Regular operating position of switch upon release of RESET CORR or actuation out of CORR OFF. |
| CORR OFF | Manually disengages SPC altitude lag compensation. |
Expand All @@ -141,4 +141,79 @@ or right.

## Throttles

TODO
![pilot_throttle](../../../img/pilot_throttle.jpg)

The throttle arrangement for each engine in the F-4E Phantom II is located on the front and rear
cockpit left console. Mechanical linkage transmits throttle movement to the engine fuel control. A
friction adjusting lever allows customization of throttle friction. Afterburner initiation occurs by
shifting the throttles outboard and moving forward from the MIL position.

Throttle movement is smooth and continuous, with afterburner modulation possible throughout the
range. Moving throttles from IDLE to OFF closes the fuel shutoff valve, stopping fuel flow. To
transition from OFF to IDLE or MIL, advance the throttles straight forward. Shifting throttles
outboard allows movement from MIL to MAX, enabling forward motion in the afterburner range.

Front cockpit throttles feature finger lifts for quick chops to IDLE, preventing inadvertent
shutoff. The lifts must be raised before retarding throttles to OFF. Rear cockpit throttles are
linked to the front cockpit, allowing only the pilot to start engines or move throttles into
afterburner range. Rear cockpit throttles can be moved from OFF without front seat assistance.

### Ignition Buttons

![IgnitionButtons](../../../img/pilot_ignition_system.jpg)

Engine ignition for startup is performed using a pair of spark plugs on each
engine, activated by pressing the red Ignition Button found on the rear of both
throttle levers. The button is depressed as part of the starting sequence to
ignite the spark plugs, initiating combustion in chambers four and five of the
engines.

### Cage Button

![pilot_cage_button](../../../img/pilot_cage_button.jpg)

In the event that
an [AIM-7](../../../stores/air_to_air/aim_7.md), [AIM-9](../../../stores/air_to_air/aim_9.md),
or [M61A1](../../../stores/guns.md) must be employed
against an airborne target with
the [sight](../../../cockpit/pilot/dcsg_controls.md#sight-mode-knob)
in A/G mode (for example, the flight is bounced by
opposing aircraft),
the [optical sight](../../../cockpit/pilot/dcsg_controls.md#sight-mode-knob)
reticle can immediately be slewed to the
Radar Boresight Line using the Cage Button, found on the inboard (right)
throttle handle. Cage mode commands the radar into BST mode with a five mile
range, and short pulse, and sets the firing circuit for the currently selected
air to air weapon relative to the Pinky Switch. For
the [optical sight](../../../cockpit/pilot/dcsg_controls.md#sight-mode-knob),
the command activates the respective elevation and azimuth tracking, roll mark, and
range functions of the reticle for the chosen weapon, without the pilot having
to remove a hand from throttle or stick to swap the sight mode or weapon control
panel functions.

### Speed Brake

![pilot_speed_brake](../../../img/pilot_air_brake.jpg)

The Speed Brakes are actuated by a three position switch found on the inboard
throttle in both cockpits. Either switch will actuate the brakes. The positions
are Out, Stop, and In; the first and last positions are momentary (reverting to
Stop upon being released).

### Dispense Button

![pilot_throttle_cm_dispense](../../../img/pilot_throttle_cm.jpg)

When pressing the dispense button chaff/flare dispensing is initiated as set on
the CCU and AN/ALE-40 programmer if the flaps and speed brakes are retracted and
the flares select switch is set to NORMAL. Additionally single unit flare
dispensing can be initiated by a single button press if the flares select switch
is set to FLARES.

### Mic Switch

![pilot_intercom_mic_switch](../../../img/pilot_inter_com_mic_switch.jpg)

The microphone switch for the Intercom System is the aft position on the inboard
throttle grip in both cockpits. When using the intercom, all audio sans the
pull-up tone, stall warning, voice warning, and ECM are reduced (same as RADIO OVERRIDE).
5 changes: 4 additions & 1 deletion src/cockpit/wso/right_console/wall.md
Original file line number Diff line number Diff line change
Expand Up @@ -10,7 +10,10 @@ suspected cases of thermal runaway.

## Autopilot Ground Test

TODO
The autopilot ground test switch, located on the No. 2 circuit breaker panel, connects external
electrical power to the AFCS circuits. It disengages if there's a loss of external power or when a
generator comes online. When operating on external power, the AFCS circuit can be deenergized by
placing the switch in the NORM (down) position.

## Instrument Ground Power

Expand Down
Binary file added src/img/pilot_throttle.jpg
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20 changes: 19 additions & 1 deletion src/intro/air_to_air.md
Original file line number Diff line number Diff line change
@@ -1,3 +1,21 @@
# F-4E Air to Air Kills

TODO
The F-4E Phantom II, an upgraded version of the F-4 Phantom series, played a significant role in
air-to-air combat during the Vietnam War. Equipped with the AIM-7 Sparrow missile, a radar-guided
weapon with beyond-visual-range capabilities, the F-4E had a notable advantage in engagements.

In Vietnam, F-4E pilots engaged in dogfights against various enemy aircraft. The Sparrow missile
allowed them to target adversaries from a distance, contributing to the aircraft's success. Key USAF
pilots, such as Steve Ritchie and Chuck DeBellevue, achieved ace status by securing five or more
air-to-air victories.

The total number of air-to-air kills attributed to the F-4E Phantom II, combining both the USAF and
USN, is estimated to be around 107 during the Vietnam War. However, this figure may vary across
sources.

Despite its effectiveness, the F-4E faced challenges in close-quarters combat due to the initial
absence of an internal cannon. Modifications, including the addition of an M61 Vulcan cannon,
addressed this limitation and improved the aircraft's performance in close-range engagements.

The success of the F-4E Phantom II in Vietnam solidified its reputation as a versatile and
formidable fighter, and it continued to serve in air forces worldwide for many years.
37 changes: 36 additions & 1 deletion src/intro/foreign.md
Original file line number Diff line number Diff line change
@@ -1,3 +1,38 @@
# F-4E Combat History in Foreign Service

TODO
The F-4E Phantom II, a stalwart in the annals of military aviation, transcended its American origins
to become a formidable force in the service of numerous foreign air forces. Its foreign deployment
was a testament to its adaptability, longevity, and indomitable presence on the global stage.

In the realm of NATO, the F-4E found itself in the arsenals of key member nations. Germany, Greece,
Turkey, and the United Kingdom incorporated the Phantom into their fleets, contributing to the
collective defense capabilities of the alliance. The F-4E's reputation for versatility and
reliability made it a linchpin in NATO's strategic posture during the tense years of the Cold War.

Venturing into the turbulent skies of the Middle East, the F-4E became a symbol of air superiority
and technological prowess. Israel, Iran, and Saudi Arabia were among the regional players that
embraced the Phantom. In the crucible of Middle Eastern conflicts, the F-4E showcased its ability to
navigate diverse operational landscapes, earning its place as a linchpin in the complex geopolitics
of the region.

Across the vast expanse of the Asia-Pacific, the Phantom's distinctive silhouette graced the skies
as it found a home in the air forces of Japan, South Korea, and Australia. Whether patrolling the
Pacific or standing ready for regional contingencies, the F-4E played a vital role in ensuring the
security of nations in the region, underscoring its adaptability to varying strategic environments.

Israel's relationship with the F-4E was particularly noteworthy. The Israeli Air Force, recognizing
the Phantom's potential, not only deployed the aircraft in conflicts but also embarked on ambitious
modification programs. These enhancements, ranging from avionics upgrades to the integration of
modern weapons systems, transformed the F-4E into a customized instrument of air power tailored to
Israel's unique security needs.

Amidst the ever-evolving landscape of military technology, foreign operators of the F-4E undertook
comprehensive upgrades and modernization efforts. These initiatives were aimed at extending the
aircraft's service life and enhancing its combat capabilities. The F-4E, with its iconic twin tails
and powerful engines, evolved to meet the demands of contemporary warfare, solidifying its place as
a venerable platform in the arsenals of its adoptive nations.

The F-4E Phantom II's foreign service was not merely a chapter in the history of military aviation
but a saga that unfolded across continents and through the corridors of geopolitical power. Its
adaptability, longevity, and combat prowess etched the Phantom into the collective memory of the
nations that flew it, leaving an enduring legacy in the skies it once dominated.
12 changes: 6 additions & 6 deletions src/stores/air_to_air/aim_7.md
Original file line number Diff line number Diff line change
Expand Up @@ -125,9 +125,9 @@ Aero-27 precludes any release, even if the round has been dropped.
The following variants of the AIM-7 family are available for this variant of the
Phantom:

| Variant | Description |
|---------|-------------|
| E | TODO |
| E-2 | TODO |
| F | TODO |
| M | TODO |
| Variant | Description |
|---------|-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|
| E | The AIM-7E Sparrow was an early version of the Sparrow missile, entering service in the 1960s. t featured semi-active radar homing guidance, relying on radar illumination from the launching aircraft for target tracking. |
| E-2 | The AIM-7E2 was an improved version of the AIM-7E, featuring enhancements to its guidance system and overall performance. It retained semi-active radar homing but included improvements to increase its effectiveness in combat. |
| F | The AIM-7F, an upgraded variant, introduced improvements in the missile's guidance system and reliability. It featured enhanced seeker technology and improved signal processing capabilities, enhancing its ability to engage targets at longer ranges. |
| M | The AIM-7M Sparrow represented a significant advancement in Sparrow missile technology and became a widely used variant. It incorporated a more advanced guidance system, including a monopulse radar seeker, which improved tracking accuracy and resistance to electronic countermeasures. The AIM-7M had a longer range compared to its predecessors, making it a versatile medium-range air-to-air missile. |
18 changes: 9 additions & 9 deletions src/stores/air_to_air/aim_9.md
Original file line number Diff line number Diff line change
Expand Up @@ -55,12 +55,12 @@ AIM-9 Launch Sequence:
The following variants of the AIM-9 family are available for this variant of the
Phantom:

| Variant | Description |
| --------- | ----------- |
| B | TODO |
| J | TODO |
| JULI | TODO |
| L | TODO |
| M | TODO |
| P | TODO |
| Captive M | TODO |
| Variant | Description |
|-----------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|
| B | The AIM-9B Sidewinder was the first operational version of the Sidewinder family, entering service in the 1950s. It utilized an infrared homing seeker for target acquisition and tracking, making it a heat-seeking missile. |
| J | The AIM-9J was an improved version of the Sidewinder, featuring enhanced guidance and performance characteristics. It retained the infrared homing seeker but had improved sensitivity and better resistance to countermeasures. |
| JULI | The AIM-9Juli, or AIM-9J "Juli," was a variant of the AIM-9J developed by Israel. It featured modifications to meet specific operational requirements. |
| L | The AIM-9L Sidewinder was a significant upgrade with improved infrared homing capabilities, allowing for better target discrimination. It introduced all-aspect targeting, meaning it could engage targets from any angle, not just from behind. |
| M | The AIM-9M represented further advancements in the Sidewinder series, with improved guidance and counter-countermeasures capabilities. It had enhanced maneuverability and improved target-tracking algorithms, making it more effective in combat situations. |
| P | The AIM-9P was a variant developed for export and used by various nations. It featured improvements over earlier models in terms of reliability and seeker performance. |
| Captive M | The Captive AIM-9M is a non-functional version of the AIM-9M Sidewinder used for training and testing purposes. |
18 changes: 16 additions & 2 deletions src/stores/air_to_ground/bombs/tv_guided_bombs.md
Original file line number Diff line number Diff line change
@@ -1,13 +1,27 @@
# TV Guided Bombs

TODO
The F-4E Phantom II was equipped with TV-guided bombs, notably the GBU-8 and AGM-62 Walleye,
enhancing its precision strike capabilities. The GBU-8, also known as the "HOBOS" (Homing Bomb
System), was a laser-guided bomb developed for the F-4E Phantom II. It featured a semi-active laser
seeker that required external laser designation from the launching aircraft or a designated
third-party source. This bomb significantly improved the F-4E's accuracy in hitting designated
targets, especially those with pinpoint precision requirements. he AGM-62 Walleye was an
electro-optical, TV-guided glide bomb employed by the F-4E. This precision-guided munition had a
television camera in its nose, allowing the pilot to visually guide the bomb to its target by
watching a live video feed. The Walleye increased the F-4E's effectiveness in attacking
well-defended and high-value targets, as it provided a "man-in-the-loop" guidance system.

Both the GBU-8 and AGM-62 Walleye were crucial additions to the F-4E's arsenal, enhancing its
ability to conduct precise strikes with reduced collateral damage. These TV-guided bombs showcased
the adaptability of the F-4E Phantom II in integrating advanced munitions to meet evolving mission
requirements.

## Variants

Available TV guided bombs include:

| Variant | Warhead |
| ----------------- | ------: |
|-------------------|--------:|
| AGM-62 Walleye I | 1000 lb |
| AGM-62 Walleye II | 2000 lb |
| GBU-8 HOBOS | 2000 lb |
Expand Down