SonicStar supersonic business jet

SonicStar supersonic business jet

June 24, 2011

SonicStar

The SonicStar supersonic business jet concept was unveiled at the 2011 Paris Air Show. The jet will be able to travel 6,000 miles at Mach 3.5, which is fast enough to make a complete circuit of the globe in under five hours.

SonicStar (4)



SonicStar (2)

SonicStar (1)

SonicStar (7)

SonicStar (6)

 

Cruising at 60,000 feet, you’ll be able to see the Earth curve underneath you, and the cabin is sized to comfortably seat 10-20 people.

High Supersonic VVIP Business Jet Aircraft:

Model Designation: SonicStar, very high supersonic business jet with quiet hybrid Electric turbine propulsion systems

Basic Description: Mid wing supersonic monoplane highly swept hybrid parabolic delta wing, parabolic leading edge, forward swept canard, fully integrated nacelles to FSSC and engines, center of mass ahead of the MAC of wing, commercial transport, VVIP 10 – 16 passenger transoceaniccontinental aircraft

Abbreviations and Acronym: Sonic (Supersonic) – STAR (Supersonic Aircraft Transport Research); S-MAGJET; Supersonic-Magnetic Advanced Generation Jet Electric Turbine.

Certified to occur in 2021 under the Federal Aviation Administration under Part 25 and new supersonics category, Part 135

Lead Certification Office (FAA, EASA)

Type Certification (Part 25 Transport Category); Commercial/civil transport

Operational Certification (Part 91, Part 135);

Special Conditions (Operation above 60,000 ft); Certification to 84,000 feet.

Design:

Standard Features; fully integrated hybrid supersonic, non-afterburning engines, hybrid aerodynamic double delta supersonic laminar flow wing design, pressurized cabin to 84,000 ft, custom-luxury cabin and pilot deck, 6000 nautical miles IFR capable range, Jet-A, JP-4 and JP-7 fuel capable, electromagnetic drag reduction technology affording dramatic reduction/elimination of sonic boom below 0.25 lbs/sq.ft., overland Mach 3.5 cruise.

Operational requirements; Hot and High altitude day conditions and landing distance 4800 ft, Class 4 operational acoustics condition compatible,

Performance requirements (mach 3.5 / 10 – 20 passengers, 60,000 ft)

Design philosophy; Create an unprecedented future supersonic aircraft which in performance, speed, range, luxury and comfort, and safety, is untouchable

Limit Speeds; Mach 3.8 due to aerothermodynamic heating and atmospheric conditions becoming of super-heated plasma species

Structure requirements; alloyed titanium 6.4V/2.8Al, co-cured and co-bonded nano-carbon composite structural sheet skins and thermoplastics

Manufacturing requirements; semi-autonomous staged production line to two aircraft per month

hypermach

By | 2017-09-03T09:25:08+00:00 Jun 24, 2011|Categories: Aviation|Tags: , |

One Comment

  1. Carlos Barrera 2014/07/03 at 11:23 pm - Reply

    Technology Submission – Novel Rotary-Turbo-InFlow Tech – Featured Development

    GEARTURBINE PROJECT
    Atypical InFlow Thermodynamic
    Technology Proposal Submission
    Novel Fueled Motor Engine Type

    *State of the art Innovative concept Top system Higher efficient percent.
    Have similar system of the Aeolipile Heron Steam device from Alexandria 10-70 AD. -New Form-Function Motor-Engine Device. Next Step, Epic Design Change, Broken-Seal Revelation. -Desirable Power-Plant Innovation.

    http://www.youtube.com/watch?v=0cPo9Lf44TE

    YouTube; * Atypical New • GEARTURBINE / Retrodynamic = DextroRPM VS LevoInFlow + Ying Yang Thrust Way Type – Non Waste Looses

    -This innovative concept consists of hull and core where are held all 8 bteps of the work-flow which make the concept functional. The core has several gears and turbines which are responsible for these 8 steps (5 of them are dedicated to the turbo stages). The first step is fuel compression, followed by 2 cold turbo levels. The fourth step is where the fuel starts burning – combustion stage, which creates thrust for the next, 5th step – thrust step, which provides power to the planetary gears and turbines and moves the system. This step is followed by two hot turbo steps and the circle is enclosed by the final 8th step – bigger turbine. All this motion in a retrodynamic circumstance effect, wich is plus higher RPM speed by self motion. The Reaction at front of the action.

    *8-X/Y Thermodynamic CYCLE – Way Steps:
    1)1-Compression / bigger
    2)2-Turbo 1 cold
    3)2-Turbo 2 cold
    4)2-Combustion – circular motion flames / opposites
    5)2-Thrust – single turbo & planetary gears / ying yang
    6)2-Turbo 2 hot
    7)2-Turbo 1 hot
    8)1-Turbine / bigger

    -With Retrodynamic Dextrogiro vs Levogiro Phenomenon Effect. / Rotor-RPM VS InFlow / front to front; “Collision-Interaction Type” – inflow vs blades-gear-move. Technical unique dynamic innovative motion mode. [Retrodynamic Reaction = When the inflow have more velocity the rotor have more RPM Acceleration, with high (XY Position) Momentum] Which the internal flow (and rotor) duplicate its speed, when activated being in a rotor (and inflow) with [inverse] opposite Turns. A very strong Novel torque power concept.

    -Non waste parasitic looses for; friction, cooling, lubrication & combustion. -Shape-Mass + Rotary-Motion = Inertia-Dynamic / Form-Function Wide [Flat] Cylindrical shape + positive dynamic rotary mass = continue Inertia kinetic positive tendency motion. Like a Flywheel.

    -Combustion 2Two continue circular [Rockets] flames. [ying yang] opposite to the other. – With 2TWO very long distance INFLOW [inside propulsion] CONDUITS. -4 TURBOS Rotary Total Thrust-Power Regeneration Power System. -Mechanical direct 2two [Small] Planetary Gears at polar position. -Like the Ying Yang Symbol/Concept. -Wide out the Rotor circumference were have much more lever [HIGH Torque] POWER THRUST. -No blade erosion by sand & very low heat target signature profile. -3 points of power thrust; 1-flow way, 2-gear, 3-turbine. *Patent; Dic. 1991 IMPI Mexico #197187 All Rights Reserved. Carlos Barrera.

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