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Venture Aeronautics Project D110 "Delta Rapier"

27.8k TheFlightGuySP  1.7 years ago

VARIANTS

D100 (No Bomb Bay | No Weapons)
D110 (9x Tactical Nuclear Ordinance)
D110 (Standard Nuclear Ordinance)
D110 (Thermonuclear Ordinance)


Overview: The Delta Rapier is a supersonic tactical/strategic nuclear bomber, capable of flying at speeds excess of Mach 3 at 75,000ft. Its payload is carried in a removable external bomb bay. It has excellent climb performance and can takeoff in a relatively short amount of time, making it ideal for quick-response nuclear strikes. It can carry a variety of small and large nuclear payloads, as well as conventional explosives. It can also be used as a low-altitude, high-speed strike bomber in the event that large nuclear payloads are unfavorable.


FLIGHT CHARACTERISTICS

Maximum Airspeed (TAS): 2100mph, 3380kph, 1825knots.
Maximum Mach: 3.2
Maximum Altitude: 90,000ft, 27,432m.
Cruising Altitude: 75,000ft, 22,860m.
Takeoff Airspeed (IAS)(Full Power): ~160mph, ~258kph, ~139knots.
Landing Airspeed (IAS): ~150mph, ~241kph, ~130knots.
Note: data values were recorded with the D100 variant, and therefore performance may change slightly depending on the payload of the other variants.
Controls:

  • VTOL: N/A
  • Trim: Trim.
  • Activate1: Engine.
  • Activate2: Airbrakes.
  • Activate3: Weapons Bay/Weapons (If Present).

NOTES

  • Do not use the airbrakes while flying at high speeds.
  • The airbrakes will result in a large pitch-up response.
  • Decreasing climb angle as you get closer to cruising altitude allows for better speed performance.
  • I recommend using about 75% Trim during the cruising phase.
  • It takes several seconds for the engine to startup. Until then throttle will not work.

GIF GALLERY


Startup Flame Effect:


Afterburner Ignition:


General Characteristics

  • Created On Windows
  • Wingspan 40.2ft (12.3m)
  • Length 74.2ft (22.6m)
  • Height 22.8ft (6.9m)
  • Empty Weight N/A
  • Loaded Weight 36,513lbs (16,562kg)

Performance

  • Power/Weight Ratio 11.14
  • Wing Loading 57.1lbs/ft2 (278.9kg/m2)
  • Wing Area 639.1ft2 (59.4m2)
  • Drag Points 2591

Parts

  • Number of Parts 297
  • Control Surfaces 0
  • Performance Cost 1,470
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    Autotag: @MrCOPTY
    Autotag: @Bo1233

    Pinned 1.7 years ago
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    @funnyplaneman
    @FlightFun

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    @BeeEngineer
    @Applefan2019
    @AirJMCAviation

    Pinned 1.7 years ago
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    @weeeeeeeeeeeeeeee
    @GabrielSatori
    @AWACSgodess

    Pinned 1.7 years ago
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    @Planebuilder2123
    @Mistral
    @ThatRandomCouchPotato

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    @Bryan5
    @KtaAviation
    @Phox

    Pinned 1.7 years ago
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    Thoughts or suggestions? Let me know!

    Pinned 1.7 years ago
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    Really nice build. +1

    +1 1.5 years ago
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    4,563 L0RR3B0RR3

    @TheFlightGuySP Oh, #Thanks

    1.6 years ago
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    @L0RR3B0RR3

    #Your Text Here
    
    1.6 years ago
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    4,563 L0RR3B0RR3

    Nice, how did you make that "big" text that you have on the biograpy?

    1.7 years ago
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    @BeeEngineer While the M50 was unable to pass Mach 1, the wing design was not the only factor.
    There have also been several examples of aircraft that had/have delta wings with straight/mostly straight trailing edges, and I can't find sufficient data suggesting that they had significant issues with it.
    So while it may present such challenges realistically, it really shouldn't present a large issue if the aircraft is aerodynamically and structurally sound.

    If you have an article regarding trailing edge flow in this manner, could you provide a link? I've been unable to find one that addressed this specifically.

    +1 1.7 years ago
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    7,074 BeeEngineer

    Nice plane though.

    1.7 years ago
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    7,074 BeeEngineer

    Supersonic aircraft like this struggle to go super sonic if the back of the wing is like this aircraft. The M-50 Bounder had this issue.

    1.7 years ago
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    57.9k Pan

    goofy ahh dassault mirage 2000👍

    1.7 years ago
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    👍👍👍👍👍👍👍👍👍👍👍👍👍👍👍👍

    +1 1.7 years ago