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  1. I thought of a way didn’t know the vasimr going on for a few yrs, like the
    particle accelerator bigger though an negative charged, with gas feeders on
    one end the other some holes for energy heated thrust to go out. Inside
    were the gas feeds into an feeds the positive charged magnetic steel, idk
    thought of things like this for a while, when huntingtrapping hiking for
    days all over the northern rockies anor forest firefighting

  2. So the only thing needed to go to Mars in 39 days is a reactor with a power
    to weight 100 times better than anything that has flown so far AND 20 000
    times the power of any reactor that has flown so far… yeah, that´ll
    happen…

    VASIMR would be great for sending robotic probes to the outer solar system
    but don´t wait around for it to get you to Mars.

  3. Im glad Dr Zubrin put the radiation issue out of the picture once and for
    all. He was correct years ago even though he got nailed for saying what he
    did. I take both sides I would like to go fast like Dr Diaz wants cutting
    the trip time and food etc BUT I would want to be safe and be able to
    return to earth if anything goes wrong on the way like using the homann
    transfer orbit or similar. So my question would be Could you not speed up
    the flight time … use the transfer but fly it faster … ? or does the
    transfer have a speed limit you may not exceed …

  4. Glad to see that dr Zubrin is on his soap box again people would be blind
    and starved by the time they returned.

  5. Vasimr is a clever use but the holy grail would be to create a
    electromagnetic engine capable of interacting with earth’s magnetic field.
    Then you wouldn’t need to eject fuel, you could just control the generated
    EM fields. The power source could be a nuclear reactor. Sadly all of the
    world’s largest electromagnets destroy themselves a few seconds after being
    fired up. If one could interact with planetary EM fields to generate
    thrust, one could also imagine using gravitational fields as guidance, like
    highways.

  6. 1:05 – 1:09 blah blah blah.. Dr. Diaz reply, soo was there a question?
    hahaha!

  7. Electric propulsion has its place. And so does chemical. Electric for cargo
    to deep space and crew from L2 to Mars/Asteroids. Chemical should be used
    to transport crew from the ground to L2 (SLS initial configuration)

  8. VASIMR’s real advantage is in its much higher power/mass as compated to
    other electric propulsion engines. It could easily handle Megawatt scale
    power compared to the kilwatt scale power that ion and hall thrusters can
    use.

    Ad Astra has a flight version that is almost completed. It is designed to
    go onto the ISS and all components are space ready. If they show that the
    flight version works in ground testing it will remove all doubt of the
    engine’s functionality.

  9. I’ve only watched the opening speech yet and it seems to me that the
    spokesperson leaves out the fact that the main advantage of VASIMR is NOT a
    higher ISP than ion engines or energy efficiency, but the “extreme” thrust
    compared to ion engines (~2.4N-5N against some millinewtons which ion
    engines can deliver). Furthermore another advantage of the VASIMR engine is
    that it can trade of thrust for higher ISP, and vise versa. We should wait
    until the VASIMR engine is fully developed and tested before we evaluate
    it. If the final version actually delivers what it promises, it would
    outshadow every form of electrical propulsion we have today.

  10. Thermal radiation; in vacuum. Lying fucking CUNT!
    Two assholes leading the assholes of the audience who believe in this
    fucking shite.
    Absolute fantacists.

  11. Dr. Zubrin, I would like to hear more about your nuclear salt-water rocket
    (or NSWR), is it feasible and could it work as a upper stage for Space X?

  12. uhhmm ahhh okay ummmh learn to speak before you criticize others oh wait i
    left out an insult.

  13. zubrin was against the bush-moon plans. now he seems angry that it got
    cancelled. I don’t follow.

  14. Where did the 200,000 kw come from? I believe it was 200 kilowatt which is
    1000 times less than the LSD fanatic is raving about. but he does have a
    point about the plasma directed back to the engine from magnetic field.
    Perhaps a cross between a pulse jet engine and the vasimir might work but
    who really gives a damn I know I don’t plan on moving to mars any time
    soon! The real reason these guys are pissed is because they now have
    competition and nobody who gets fed chicken wants to end up eating the
    feathers 

  15. whats with the light on the projector screen.
    thanks for the straight forward info RZ :)

  16. Fair Warning: Moderated Wall O’ Text, Formal Rant Inbound

    In honesty, the VASIMR concept is a great one but its practicality is still
    far flung.

    Dr. Zubrin has always had this ‘ranting’ front about him, but he makes good
    points, has experience and his share of bad points. I do believe he has
    some misguided disagreement to the Ad Astra team for some of their numbers,
    considering the media blew it out of proportion (And we know how the media
    likes to twist #s)

    To start off, his main point is that we don’t need VASIMR to get to Mars,
    we can do it with existing tech and without Govt scape goats of “we need
    new tech so we can fund it”

    -Yes the Govt is looking for scape goats so they can delay missions due to
    funding.
    -Yes VASIMR requires a high power source (Ad Astra admitted to this)
    -Yes you run the risk of diverging plumes if you can’t balance exhaust
    velocity with Thrust (Remember higher exhaust velocity equals lower thrust,
    and you need high velocity to escape those B field lines depending upon the
    B-field strength)
    -Yes efficiency in VASMIR’s subsystems (RF generator, B Field couplers,
    etc) is an issue that needs/has-been to be addressed.
    -Yes without large amounts of coolant, you can’t do long burns with VASIMR

    Notes: Average Close Encounter Distance Earth->Mars ~82.2 million km. In 39
    days, you’d need a transit velocity of ~24335 m/s. For comparison, Deep
    Space One (A Ion Drive Probe) had a velocity of ~4291m/s with an Isp of
    ~2500s, covering a distance of ~180 million km in a timespan of Oct ’98 to
    July ’99 (~9 Months). I know this is an apples-to-oranges comparison,
    however we have to be grounded to *what is feasible* in terms of transit
    time.

    His cons however are as stated:
    -He has not done his fair share of digging in the numbers, Ad Astra has
    developed 100kW VASIMR rockets
    -His follow up speaker makes mention of pulsating the magnetic field to
    save on coolant.

    For as much “butthurt & ranting” as Dr. Zubrin may seem, he still makes
    *realistic* points about this type of propulsion that some people need to
    come back to the ground and realize “We need not build these large crafts
    to get us there, when we can moderate and be smart about how and what we
    use to get us *there* “

  17. I think the VASIMR rocket concept is quite normal, and it isn’t really a
    hoax unless the people building it have deceptive motives. I think a
    next-generation nuclear powered spacecraft is a wonderful technology in the
    hands of the Bourgeois…

  18. Is the VASIMR ion thrusters technology related to David LaPoint’s
    explanation of plasma jets stream on both magnetic pole direction as shown
    in his work on “The Primer Fields”?

  19. in the long run the answer is of course fusion. Either a direct fusion
    drive or a reator running on the proton Boron-11 reaction cycle. And the
    reactor will have to be one of the non Tokamak types if, a big if they can
    get them to work

  20. Is there even any point having a manned spaceflight program anymore in the
    US? No manned mars mission is going to get funding this side of 2040, and
    the only reason even SLS exists is because of the need to placate key
    businesses and Florida.

  21. Instead of turning to kindergarten level debating skills, why don’t you try
    to point where and how I am wrong.

  22. True, and the VASIMR folks have wisely not mentioned that. I was replying
    to the observation that some were talking about 500 day burns in
    interplanetary transits. And I should have said interstellar “burns” will
    take over a year. Obviously the transit will take over a year. But anyway,
    the point made was that VASIMR is low power and needs to burn long to get a
    good delta v. But the key problem is specific power and the mass of the
    primary mover.

  23. this is stupid! VASIMR should be given a chance because moon projects won’t
    get humanity anywhere it already hasn’t.

  24. The AdAstra Company responsible for the VASIMIR sure has a lot of people
    fooled. We could use a NTR and get twice the efficiency of our best
    chemical rockets. In fact such rockets are under development in Russia
    today.

  25. The problem is that future propulsion systems are indeed needed for future
    missions, we can’t expect to rely on chemical propulsion forever. In the
    30’s the Allies wheren’t interested in building jet propulsion ’cause they
    thought existing propeller driven planes where all they would ever need.
    Its only when the Germans created the 1st jet fighter that they realized it
    was a big mistake to not try and develop a better propulsion system. Now
    today jet propulsion is everywhere.

  26. @aurora7207 No need to argue that point, I agree. I just use it as the
    example simply because it is the most dominant and influential globally
    (and it’s the one that’s directly related to this (Mars Society)). But, it
    actually goes even deeper to our root notions of value and ownership.
    Peeking at your channel I can see we share a common outlook. If you head
    over to my channel I think you’ll find some vids you might enjoy.

Mars in 39 Days?: the VASIMR Plasma Engine. Franklin Chang-Diaz, Ph.D.

From DDP 31st Annual Meeting, July 13, 2013, Houston, TX. Dr. Franklin Chang Diaz is founder and current CEO of Ad Astra Rocket Company, www.adastrarocket.com, a U.S. firm developing advanced plasma rocket technology with operations in Houston, Texas, and Guanacaste, Costa Rica. In 2005 Dr. Chang Díaz completed a 25-year career as a NASA astronaut, where he became a veteran of 7 space missions. He has logged more than 1,600 hours in space, including 19 hours in three space walks. In 1994, in conjunction with astronaut training at NASA, he founded and directed the Advanced Space Propulsion Laboratory (ASPL) at the Johnson Space Center, where he managed a multi-center research team developing advanced plasma rocket propulsion concepts. Dr. Chang Díaz is the inventor of the VASIMR® engine, a high-power plasma rocket currently under development by Ad Astra for in-space applications. He has more than 30 years of experience in experimental plasma physics, engineering, and high-power electric propulsion and 25 years of experience in space operation and the management and implementation of research and development programs at NASA. Dr. Chang Díaz holds a Ph.D. degree in applied plasma physics from the Massachusetts Institute of Technology and a Bachelor of Science degree in mechanical engineering from the University of Connecticut. Prior to his work at NASA, Dr. Chang Díaz was involved in magnetic and inertial confinement fusion research at MIT and the Charles Stark Draper Laboratory. He is an adjunct professor of physics at Rice University and the University of Houston.