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Friday, January 29th, 2016  |  USD: Buy 531.29 / Sell 543.92
20 years

Costa Rican scientist’s plasma engine ready for space

chang plasma engine

February 20th, 2013 (InsideCostaRica.com) Costa Rican scientist and astronaut, Franklin Chang, is about to fulfill a dream.

 

His plasma engine, known as the Variable Specific Impulse Magnetoplasma Rocket, or VASIMR, first imagined three decades ago to make space travel faster and cheaper, is almost ready.

 

Director of Ad Astra Rocket Costa Rica, Ronald Chang, said that the only thing left is to launch and test the engine in space.

 

Chang’s mother, Maria Eugenia Diaz, said that she is very proud to see her child’s achievement.

 

Recently the Costa Rican Aerospace Alliance announced their support of the project by developing an exterior support device for the Chang’s engine to be fitted on the exterior of the International Space Station, as part of the plan to test the VASIMR in space. This test phase is now expected to be conducted in 2014.

 

The engine could reduce the duration of flight from Earth to Jupiter or Saturn from six years to fourteen months, and Mars from 4 months to 39 days.

 

Getting the engine into space for testing could cost up to $80 million.

 

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  • http://works.bepress.com/retrodynamic/1/ RETRODYNAMIC

    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.

    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..

    -Combustion 2Two continue circular [Rockets] flames. [ying yang] opposite one 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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