机型库Lockheed F-117A Nighthawk

Staff Sgt. Aaron Allmon II · Public domain · F-117 Nighthawk Front.

Lockheed F-117A Nighthawk

A single-seat, twin-engine stealth attack aircraft developed by Lockheed.

Military jet配置文件选项：1 个

了解飞机

Lockheed developed the F-117A to attack high-value targets while reducing radar detection. Its low-observable design was the basis of the first operational stealth aircraft. A single pilot operates the aircraft, powered by two General Electric F404-F1D2 engines.

Crew: One↗
Engines: Two General Electric F404-F1D2↗

USAF Museum F-117A reference

Wingspan: 43 ft 4 in↗
Length: 65 ft 11 in↗
Maximum weight: 52,500 lb↗
Internal stores capacity: 5,000 lb↗

在 AirframeDB 上了解这款航空器

Low-observable development and a test-aircraft survivor

Developed around reducing detection by radar, the F-117A first flew on 18 June 1981. The 4450th Tactical Group reached initial operating capability in October 1983, several years before the aircraft became publicly familiar. Its first combat use was in Panama in December 1989, followed by the Gulf conflict of 1990–1991.

The National Museum of the USAF records 59 production aircraft built between 1981 and 1990. Its exhibit is the second F-117A, used for development testing from 1981 to 1991. That individual history explains why a museum airframe can represent the programme’s experimental work rather than a front-line combat career.

Pitch commands and Mach hold

The 2023 MSFS 2020 guide describes +6G and -2G commands at full aft and forward stick. Mach hold changes pitch to maintain Mach; altitude, heading and destination/navigation hold are also documented.

公开来源 4

Lockheed F-117A NighthawkMuseum aircraft history and technical notes
F-117A User Guide — version 1.225 June 2023 · MSFS 2020 guide
F-117 Nighthawk for Microsoft Flight SimulatorOriginal MSFS product · checked 11 October 2026
F-117 Nighthawk for Microsoft Flight Simulator 2024Separate MSFS 2024 product · checked 11 October 2026

配置文件如何建模

Lockheed F-117A Nighthawk

Free + Pro

MSFS 2020MSFS 2024Aerial Simulations

Aerial Simulations has separate original MSFS and MSFS 2024 products. The preserved June 2023 version 1.2 guide describes the MSFS 2020 implementation.

The 0.55 baseline spring has no low-speed blend or high-speed stiffening. A small 0.04 aerodynamic-load term uses a 300-KIAS reference; these are inherited force estimates.

Trim relief and local force trim are off. Gear-motion texture remains enabled, while flap, spoiler, reverse-thrust and engine-vibration cues are disabled.

此确切修订版尚未开放公开安装。

Controls and trim

The MSFS 2020 guide describes +6G at full aft stick and -2G at full forward stick, with angle-of-attack limits. These commanded-load values describe the add-on’s pitch logic. The profile’s fixed-centre spring and damping remain estimates rather than a measured F-117 force law.

F-117A User Guide — version 1.2

Equipment cues

The product listings include radar-cross-section monitoring, custom Mach hold, a drag chute and exterior animations. Gear-motion texture uses observed movement. No carrier, catapult or afterburner effect is introduced.

F-117 Nighthawk for Microsoft Flight Simulator F-117 Nighthawk for Microsoft Flight Simulator 2024

Autopilot

The guide’s autopilot has altitude, pitch-based Mach, heading and destination/navigation modes. Mach hold changes pitch rather than throttle. The guide does not publish calibrated servo targets, so physical autopilot following and neutral hold stay off.

F-117A User Guide — version 1.2

About the values

Gains are normalized profile estimates. Physical hand force depends on the device and its output limits. Indicated-speed references are tuning scales; physical acceptance of revision 2 remains pending.

Master gain & control system

Master gain85%

施加于模型产出的一切、在设备上限之前的最终整体输出缩放。

调高: 一切(弹簧、载荷、效果)一同增强。

调低: 一切一同变柔。

设定理由: Scales overall profile strength while preserving effect balance, subject to device and output limits.

Forces

Spring strength55%

把摇杆拉回中央的基础回中力。其他所有力都叠加在它之上。太低,正常飞行中摇杆会发软;太高,它会与你的手较劲,并掩盖叠加其上的细微提示。

调高: 更硬的回中,更抗手。

调低: 更软的杆,只靠气动载荷。

设定理由: The inherited 0.55 spring supplies a fixed centre. Low-speed airspeed blending and high-speed stiffening are disabled.

Spring deadband4%

中央附近弹簧保持安静的小中立区,让静止时的微小移动不会咔嗒作响。更宽更安稳但更松,更窄更精确但可能在中央附近抖动。

调高: 更安静但更松的中央,旷量更大。

调低: 更紧的中央,静止时可能抖动。

设定理由: Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.

Overall aerodynamic load4%

作用于两条持续轴载荷的主缩放,在它们各自的独立平衡之前施加。配置文件通常不动它,而是调校两条轴载荷。

调高: 两轴载荷一同加重。

调低: 两轴一同减轻。

设定理由: The 0.04 gain adds a small aerodynamic-load term alongside the fixed-centre spring. It does not reproduce the guide’s commanded-G law.

Airspeed blendingFalse

启用低速弹簧介入窗口(上面的起始/全强度节数)。关闭时弹簧在所有速度下恒定。

设定理由: Allows baseline spring strength to rise with indicated airspeed where the control law permits it.

Low-speed spring floor50%

在静止、空速尚未产生气动力之前,弹簧还剩多少。下限高,停机时摇杆结实;下限低,则是停放轻型飞机那种钢索松弛的感觉。

调高: 停机和滑行时杆更结实。

调低: 停机时杆发软,只随速度苏醒。

设定理由: Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.

Spring engagement start20 kt

弹簧从低速下限开始向全强度攀升的空速:起飞滑跑中操纵面"苏醒"的那一刻。

设定理由: Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.

Spring engagement full90 kt

弹簧达到全强度的空速。从起点到这里,随着气流在操纵面上增强,回中逐渐变硬。

设定理由: Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.

力反馈调校速度300

气动载荷达到设计满值的指示空速。它把整条载荷曲线锚定在飞机真实的速度范围:172在110节就载满,喷气机要晚得多。

调高: 载荷来得更晚;杆轻到更高速度。

调低: 载荷来得更早,巡航更沉。

设定理由: The retained 300-KIAS reference is the profile’s aerodynamic load scale; it is not a published F-117 cruise speed or limit.

Centre firmness vs speed0%

在偏转载荷之外,回中本身随速度变硬的程度。零则中央手感恒定;越大,巡航时回中越硬,起落航线上越松。

调高: 中央随速度明显变硬。

调低: 任何速度下中央手感恒定。

设定理由: Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase.

Centre stiffening cap5

速度驱动的中央变硬上限,防止高速飞行把弹簧无限上紧。

调高: 高速允许更多总硬化。

调低: 硬化更早封顶。

设定理由: Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.

Aileron load100%

由副翼偏转和空速产生的持续横滚载荷,独立于俯仰调校。与升降舵载荷一起,决定评测中常说的操纵协调比。

调高: 横滚力更重。

调低: 副翼更轻更灵。

设定理由: Scales roll aerodynamic loading. The separate roll spring curve also affects total axis balance.

Elevator load100%

由升降舵偏转和空速产生的持续俯仰载荷,独立于横滚调校。这是决定机型俯仰重量的主杠杆。它不影响副翼、弹簧、配平或抖振力。

调高: 速度下持续俯仰力更重。

调低: 升降舵更轻,握持更省力。

设定理由: Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.

Max output force55%

每个稳态俯仰或横滚力到达设备前的上限,防止猛烈机动中砸击或饱和硬件。

调高: 削波前更高的稳态力峰值。

调低: 更柔的上限;猛烈机动更早被抹平。

设定理由: Caps directed-force output. Native spring effects and device limits remain separate.

Trim

Trim relief (elevator)30%

升降舵配平缓解持续俯仰力、移动杆的安定位置的强度。在100 %时,配平得当的飞机不需要保持压力——正是真实飞行中"用配平消掉载荷"的流程。

调高: 配平消掉更多持续力;100 %时满配平可完全抵消。

调低: 即使配平也仍要持续用力。

设定理由: The stored pitch authority is inactive because trim relief is disabled; simulator trim does not move the hardware neutral through this effect.

Trim relief (aileron)30%

横滚配平的同类缓解。多数通航机型没有真正的副翼配平,所以保持为零;有横滚配平的机型获得相应的值。

调高: 横滚配平消掉更多持续力。

调低: 横滚配平作用更小。

设定理由: Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.

Effect gains · Ground

Runway rumble36%

由轮速和地面类型(铺装、草地、砾石)产生的滚动振动。

调高: 杆上更强的地面质感。

调低: 更平滑的滑行。

设定理由: Sets rolling texture strength, modified by speed, surface and undercarriage configuration.

Gear bumps30%

来自伸缩缝、车辙和粗糙地面的短促离散颠簸,为持续隆隆声打上标点。

调高: 接缝与车辙的冲击更清晰。

调低: 更柔的地面细节。

设定理由: Sets gear-bump texture during ground motion, separate from touchdown impact.

Effect gains · Airframe

Stall buffet15%

接近失速及失速警告响起时的机体抖动:这副机翼宣告不满的音量。断失干脆的机型抖振收敛,让喇叭承担警告。

调高: 更强的失速前颤抖。

调低: 更含蓄的机翼;警告交给喇叭。

设定理由: Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.

Mach buffet0%

接近马赫极限的跨音速抖振。对接近MMO的喷气机有意义,对到不了那里的活塞机和涡桨机为零。

调高: 接近马赫极限时更强的跨音速抖振。

调低: 高马赫下更平滑的飞行。

设定理由: Sets high-Mach buffet strength; onset and full-strength thresholds are separate.

Flap buffet0%

襟翼伸入气流后机体的低频振动,发生在它们真正做功的速度窗口内。

调高: 襟翼做功时更粗糙的飞行。

调低: 更柔的进近襟翼。

设定理由: Flap buffet is disabled; conventional flap behavior is not inferred from the shared force parent.

Gear buffet10%

可收放起落架悬在气流中引起的机体鼓振。固定起落架机型为零,它们的机体外形从不改变。

调高: 放起落架时更多鼓振。

调低: 放起落架飞行更干净。

设定理由: Sets gear aerodynamic buffet; movement and ground-contact cues are separate.

Stick shaker50%

由飞机自身失速警告系统触发的专用抖杆器振动。只有真有抖杆器的机型才有值;其余全靠气动抖振和喇叭。

调高: 更硬的抖杆器。

调低: 更含蓄的抖杆器。

设定理由: Sets triggered shaker strength; inactive while the shaker feature is disabled.

Spoiler buffet0%

速度中展开的扰流板或减速板带来的抖动。没有的机型为零。

调高: 扰流板展开时更多晃动。

调低: 更含蓄的扰流板。

设定理由: Spoiler buffet is disabled; a spoiler cue is not inferred from the shared force parent.

Effect gains · Engine, mechanical & drag

Touchdown thump88%

机轮触及跑道那一下的单次冲击,按下沉率缩放:轻柔着陆是耳语,结实到达是一记闷响。

调高: 触地时更硬的一击。

调低: 更柔的到达。

设定理由: Sets landing-impact strength; landing telemetry and response shape determine the pulse.

Reverse rumble0%

反推或桨叶beta区工作时的滑跑振动。无反推机型为零。

调高: 反推下更粗糙的滑跑。

调低: 更含蓄的反推。

设定理由: Reverse-thrust vibration is disabled.

Engine rumble0%

从慢车到全功率跟随转速的持续动力装置振动——前方有东西在烧油的永恒提醒。

调高: 杆里更多发动机。

调低: 更含蓄的发动机。

设定理由: Engine rumble is off, alongside simulator engine-vibration following. No measured F-117 engine or afterburner vibration is assigned.

Flap motion0%

仅在模拟器报告襟翼舵面确实移动时的持续振动。它跟随真实作动器的运动和故障,而非估算的计时器。

调高: 襟翼移动中更多振动。

调低: 更含蓄的襟翼行程。

设定理由: Flap-motion texture is disabled.

Flap drag0%

襟翼阻力在速度中带来的持续俯仰力变化。放襟翼应该改变你手里握着的东西,而不只是发出声音。

调高: 放襟翼时更大的力变化。

调低: 襟翼引起的配平漂移更少。

设定理由: This independently configured effect remains subject to valid simulator telemetry and bounded device output.

Spoiler drag0%

展开扰流板带来的持续载荷变化。没有的机型为零。

调高: 扰流板更大的载荷变化。

调低: 更少。

设定理由: This independently configured effect remains subject to valid simulator telemetry and bounded device output.

Flap detent click0%

襟翼手柄每个卡位上短促的机械咔嗒。是手柄,不是舵面。

调高: 更清脆的卡位咔嗒。

调低: 更轻的咔嗒。

设定理由: Discrete flap-step texture is disabled.

Flap arrival0%

襟翼舵面行程完成时机体的轻微安定,由舵面到位驱动,而非手柄指令。

调高: 到达卡位时更结实的安定。

调低: 更柔的到位。

设定理由: Flap-arrival texture is disabled.

Autopilot follow

AP follow authority5%

自动驾驶指令可以让杆实际移动多远。在MSFS中保持极小,因为移动的轴可能被读回为飞行员输入;零则完全禁用跟随。

调高: 自动驾驶让你的杆移动得明显更多。

调低: 几乎察觉不到的跟随。

设定理由: Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.

Stick feel

StickFeel · Trim feel enabledFalse

Whether this feature is active in this profile.

设定理由: Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.

StickFeel · Trim relief enabledFalse

Whether this feature is active in this profile.

设定理由: Trim relief is disabled. The guide’s simulator trim adjustment does not establish a physical neutral-to-trim relationship.

StickFeel · Force trim enabledFalse

Whether this feature is active in this profile.

设定理由: Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.

StickFeel · G load enabledFalse

Whether this feature is active in this profile.

设定理由: Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.

StickFeel · Rate damping enabledTrue

Whether this feature is active in this profile.

设定理由: Enables rate damping with the configured coefficients and control law.

Autopilot

Autopilot · Follow enabledFalse

Whether this feature is active in this profile.

设定理由: The guide’s autopilot has altitude, pitch-based Mach, heading and destination/navigation modes. Mach hold changes pitch rather than throttle. The guide does not publish calibrated servo targets, so physical autopilot following and neutral hold stay off.

Autopilot · Neutral hold enabledFalse

Whether this feature is active in this profile.

设定理由: Permits centering hold during a supported AP state, separate from following a moving target.

Autopilot · Neutral hold strength0.6

设定理由: Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.

Aero

Aero · EnabledTrue

Whether this feature is active in this profile.

设定理由: Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.

Aero · Max flap index2

Where this effect reaches full strength (or has fully faded, for washouts).

调高: a more gradual build to a later peak.

调低: a quicker build.

设定理由: Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.

Aero · Min flap index2

Where this effect begins fading in.

调高: the effect begins later.

调低: it begins earlier.

设定理由: Sets the first flap detent that admits buffet; this is a handle index, not degrees.

Aero · Shaker enabledFalse

Whether this feature is active in this profile.

设定理由: Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.

Ground

Ground · EnabledTrue

Whether this feature is active in this profile.

设定理由: Enables ground effects; each still needs its own strength and contact or motion telemetry.

Engine

Engine · EnabledFalse

Whether this feature is active in this profile.

设定理由: Enables engine cues with nonzero settings and valid running-engine telemetry.

Mechanical

Mechanical · EnabledTrue

Whether this feature is active in this profile.

设定理由: Enables accessory cues with configured strengths and observed accessory movement.

Mechanical · Gain0.12

The strength of this effect.

调高: a stronger effect.

调低: a weaker one.

设定理由: Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.

Stick alive

StickAlive · EnabledFalse

Whether this feature is active in this profile.

设定理由: This independently configured effect remains subject to valid simulator telemetry and bounded device output.

Sim engine vibrationFalse

在可用时使用模拟器自身的发动机振动信号,而非合成的隆隆声。

设定理由: This independently configured effect remains subject to valid simulator telemetry and bounded device output.

Hydraulics

Hydraulics · Loss load increase0

设定理由: Hydraulic-loss loading is zero. An aircraft-specific F-117 failure-to-inceptor response has not been established.

全部配置文件设置

估算的配置文件设置
参数	数值	控制作用及原因
Spring strength	0.55	The inherited 0.55 spring supplies a fixed centre. Low-speed airspeed blending and high-speed stiffening are disabled.
Spring deadband	0.04	Sets travel around the centre before the baseline spring resists. Smaller values engage it sooner.
Force gain	0.04	The 0.04 gain adds a small aerodynamic-load term alongside the fixed-centre spring. It does not reproduce the guide’s commanded-G law.
Master gain	0.85	Scales overall profile strength while preserving effect balance, subject to device and output limits.
Dynamic-pressure blend	False	Allows baseline spring strength to rise with indicated airspeed where the control law permits it.
Minimum spring factor	0.5	Sets low-speed spring strength as a fraction of baseline when blending is enabled. One keeps full strength.
Spring wake-up speed	20 kt	Sets the IAS where the low-speed spring blend starts rising. This is a feel threshold, not a flight limit.
Spring full-strength speed	90 kt	Sets the IAS where the low-speed blend reaches baseline strength; high-speed stiffening also uses it.
力反馈调校速度	300.0 kt	The retained 300-KIAS reference is the profile’s aerodynamic load scale; it is not a published F-117 cruise speed or limit.
Airspeed spring stiffening	0	Adds permitted spring resistance above the full-blend speed. Zero removes this high-speed increase.
Airspeed stiffening cap	5	Limits the squared airspeed ratio used for high-speed spring stiffening; it is not a device-force cap.
Aileron force scale	1	Scales roll aerodynamic loading. The separate roll spring curve also affects total axis balance.
Elevator force scale	1	Scales pitch aerodynamic loading; pitch spring travel and trim responses are separate settings.
Maximum output force	0.55	Caps directed-force output. Native spring effects and device limits remain separate.
StickFeel · Trim feel enabled	False	Retained for compatibility and group membership. Trim relief, rather than this flag, controls centre movement.
StickFeel · Trim relief enabled	False	Trim relief is disabled. The guide’s simulator trim adjustment does not establish a physical neutral-to-trim relationship.
StickFeel · Elevator authority	0.3	The stored pitch authority is inactive because trim relief is disabled; simulator trim does not move the hardware neutral through this effect.
StickFeel · Aileron authority	0.3	Scales supported roll-trim relief and permitted centre movement. Zero removes roll response.
StickFeel · Force trim enabled	False	Enables local force trim, separate from aircraft-owned trim and add-on integration qualification.
StickFeel · G load enabled	False	Allows load-factor changes to modify permitted spring laws. Passive fly-by-wire feel can suppress it.
StickFeel · Rate damping enabled	True	Enables rate damping with the configured coefficients and control law.
Autopilot · Follow enabled	False	The guide’s autopilot has altitude, pitch-based Mach, heading and destination/navigation modes. Mach hold changes pitch rather than throttle. The guide does not publish calibrated servo targets, so physical autopilot following and neutral hold stay off.
Autopilot · Follow authority	0.05	Sets admitted AP-follow gain, not a percentage of travel. Runtime ownership and input limits still apply.
Autopilot · Neutral hold enabled	False	Permits centering hold during a supported AP state, separate from following a moving target.
Autopilot · Neutral hold strength	0.6	Sets admitted AP neutral-hold strength; inactive while neutral hold is disabled.
Aero · Enabled	True	Enables aerodynamic cues; each still needs nonzero strength and its simulator conditions.
Aero · Gain	0.15	Sets stall-buffet strength. Zero removes the cue without changing simulator stalls or warnings.
Aero · Gain	0	Sets high-Mach buffet strength; onset and full-strength thresholds are separate.
Aero · Gain	0	Flap buffet is disabled; conventional flap behavior is not inferred from the shared force parent.
Aero · Max flap index	2	Sets the final flap index for detent normalization. UP plus three detents uses maximum index3.
Aero · Min flap index	2	Sets the first flap detent that admits buffet; this is a handle index, not degrees.
Aero · Gain	0.1	Sets gear aerodynamic buffet; movement and ground-contact cues are separate.
Aero · Shaker enabled	False	Permits shaker at supported warning conditions; the switch does not establish aircraft equipment.
Aero · Amplitude	0.5	Sets triggered shaker strength; inactive while the shaker feature is disabled.
Ground · Enabled	True	Enables ground effects; each still needs its own strength and contact or motion telemetry.
Ground · Gain	0.36	Sets rolling texture strength, modified by speed, surface and undercarriage configuration.
Ground · Gain	0.3	Sets gear-bump texture during ground motion, separate from touchdown impact.
Ground · Gain	0.88	Sets landing-impact strength; landing telemetry and response shape determine the pulse.
Ground · Gain	0	Reverse-thrust vibration is disabled.
Engine · Enabled	False	Enables engine cues with nonzero settings and valid running-engine telemetry.
Engine · Gain	0	Engine rumble is off, alongside simulator engine-vibration following. No measured F-117 engine or afterburner vibration is assigned.
Mechanical · Enabled	True	Enables accessory cues with configured strengths and observed accessory movement.
Mechanical · Gain	0	Flap-motion texture is disabled.
Mechanical · Gain	0.12	Sets texture from observed gear movement, separate from aerodynamic and touchdown effects.
StickAlive · Enabled	False	This independently configured effect remains subject to valid simulator telemetry and bounded device output.
StickAlive · Use sim engine vibration	False	This independently configured effect remains subject to valid simulator telemetry and bounded device output.
Hydraulics · Loss load increase	0	Hydraulic-loss loading is zero. An aircraft-specific F-117 failure-to-inceptor response has not been established.
Aero · Gain	0	Spoiler buffet is disabled; a spoiler cue is not inferred from the shared force parent.
AeroDrag · Gain	0	This independently configured effect remains subject to valid simulator telemetry and bounded device output.
AeroDrag · Gain	0	This independently configured effect remains subject to valid simulator telemetry and bounded device output.
Mechanical · Gain	0	Discrete flap-step texture is disabled.
Mechanical · Gain	0	Flap-arrival texture is disabled.

公开来源 4

Lockheed F-117A NighthawkMuseum aircraft history and technical notes
F-117A User Guide — version 1.225 June 2023 · MSFS 2020 guide
F-117 Nighthawk for Microsoft Flight SimulatorOriginal MSFS product · checked 11 October 2026
F-117 Nighthawk for Microsoft Flight Simulator 2024Separate MSFS 2024 product · checked 11 October 2026

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