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Space

Private Rocketplane Test A Success 283

HobbySpacer writes: "XCOR announced the success of the first phase of flight tests for the EZ-Rocket. In the most recent flight, Dick Rutan fired both of its rocket engines to take off and reach a speed of 160knots and an altitude of 6200 feet. The vehicle is a Long-EZ kit plane modified to hold twin 400 lb thrust rocket engines fueled by isopropyl alcohol and liquid oxygen. The project is not aimed at a homebuilt EZ-Rocket but will demonstrate safe and reliable rocket propulsion. The primary goal is development of reusable launch technology that leads next to a high altitude sub-orbital rocket vehicle for space tourism, rocket racing (e.g. vertical drag racing at air shows) and the X-Prize competition."
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Private Rocketplane Test A Success

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  • Unit conversions (Score:3, Informative)

    by metricman ( 265010 ) on Thursday October 04, 2001 @11:57PM (#2390826)
    160knots = 296 km/h
    6200 feet = 1890m
    400 lb = 1779N

    A cool feature for slashcode would be automatic unit conversions.
  • by jeboyer ( 24453 ) on Friday October 05, 2001 @12:40AM (#2390948)
    "The primary issue with getting into orbit isn't going up, its with going sideways at around 17,000 mph."

    True. On the other hand, there are definite advantages to getting above a high percentage of that pesky thick layer of air that seems to blanket this planet.

    * There's a lot of aerodynamic drag associated with the passage through the dense atmosphere at low altitudes Ever notice the Shuttle and other rockets throttle down at the "max Q" (maximum aerodynamic pressure) point? That (inefficient) action is necessary to limit the forces so the vehicle won't break up.

    * Although the altitude balloons can reach is much, much less than that of orbit, there is still a measurable advantage in necessary delta-v (velocity increment needed to reach orbit) from a high-altitude launch. I haven't look at the exact numbers in years, but it's on the order of percents--not insignificant when dealing with the tight margins inherent in launching.
  • by Gorobei ( 127755 ) on Friday October 05, 2001 @12:47AM (#2390964)
    The main reason is the FAA. If you want to be a high alt attempt, you need to file a lot of paperwork concerning your flight plan and risks to populated areas/foreign airspace. In theory, you could get approval for an orbital shot from two places in the USA (Black Rock and Alaska,) if you have a self-destruct device on board. Note that a self-destruct doesn't make the rocket vanish, it just puts the debris in a safe zone. Now, if you want to float to 120,000 feet before launch, your debris zone is about the size of the Pacific Ocean. You don't get approval, end of story.
  • Rotary Rocket gone (Score:3, Informative)

    by Animats ( 122034 ) on Friday October 05, 2001 @01:28AM (#2391019) Homepage
    Rotary Rocket is gone. Sad. They had a launch vehicle that was supposed to go suborbital, and probably would have worked. The helicopter-type landing system passed flight test. Another Rutan airframe design, by the way. [rotaryrocket.com]

    The big problem was that the new engine concept didn't work out, and using off the shelf engines doomed the thing to suborbital flight, for which there is no commercial market.

  • by Chris Y Taylor ( 455585 ) on Friday October 05, 2001 @01:45AM (#2391046) Homepage
    I think you are refering to a "rockoon".

    http://www.friends-partners.org/mwade/lvs/rockoo n. htm

    They were invented by Dr. Van Allen and some of his associates. They were only for sounding rockets, which explore the upper atmosphere but don't go into orbit. If you want to go into orbit, you still need a lot of horizontal velocity so the rockoon is not as handy for that.
  • article text (Score:2, Informative)

    by FrenZon ( 65408 ) on Friday October 05, 2001 @02:03AM (#2391071) Homepage
    it seems like the server's going down (or it could just be australia's crap old ADSL) So here's the body text, fear my karma-whoring or something.

    Mojave, October 3, 2001: XCOR Aerospace today announced that it has successfully completed the first phase of its flight test program for the EZ-Rocket. The EZ-Rocket is the world's first privately built rocket powered airplane.

    At 0900 hours today the EZ-Rocket took off from the Mojave Civilian Flight Test Center to an altitude of 6,200 feet before gliding back to Runway 30. The EZ-Rocket is powered by twin 400 pound thrust rocket engines designed and built by XCOR Aerospace. The flight test program passed its first milestone by flying with both engines for an engine run time of 96 seconds and total flight time of five minutes and twenty seconds.

    Retired United States Air Force Lieutenant
    Colonel Dick Rutan


    XCOR's test pilot is retired United States Air Force Lieutenant Colonel Dick Rutan, a Vietnam veteran and world-famous test pilot. "I ignited one engine and the crew said everything looked good, so I lit the second engine and we started moving," said Lt. Col. Rutan. "As I rolled down the runway Mike Melvill flew overhead in another Long-EZ and served as chase plane. The plane took off 1,200 feet down the runway and once airborne the vehicle rapidly accelerated to 160 knots. The rocket power provided positive, firm acceleration. Once we started running out of liquid oxygen I shut down both engines. Mike inspected the airplane visually and reported it was clean with no leaks. We entered a standard flame-out [landing] pattern and glided back to the runway."

    The EZ-Rocket is a research and development test bed for XCOR. "Routine operations must be the primary criterion for rocket engine development," said XCOR Chief Engineer Dan DeLong. "Our approach is to build safe and reliable rocket engines first, then progress to the higher performance needed for orbital launch vehicles."

    XCOR president Jeff Greason said, "We passed a major milestone today. This is a significant technical achievement for a variety of reasons. First, once you get two engines working in combination it is significantly easier to cluster more engines for larger vehicles. Second, we were able to keep the engine and fuel flow running smoothly during the flight."

    The official roll-out and flight demonstration of the EZ-Rocket will take place this November at Mojave airport. Check the XCOR (www.xcor.com) web site in the next few days for details on the event.

    EZ-Rocket Specifications
    The EZ-Rocket is a modified Long-EZ homebuilt aircraft. The aircraft is powered by twin 400 lb thrust regeneratively cooled rocket engines and fueled by isopropyl alcohol and liquid oxygen. The EZ-Rocket includes an external composite fuel tank and an insulated internal aluminum liquid oxygen tank. The modifications were performed at XCOR Aerospace's Mojave, CA shop. Tests are performed at the Mojave Civilian Flight Test Center.

  • by maetenloch ( 181291 ) on Friday October 05, 2001 @02:45AM (#2391130)
    JP Aerospace [jpaerospace.com] "America's OTHER Space Program" is doing this very thing. They used balloons to carry a launch platform and rocket to 26,000 ft where they launched the rocket. Now they're currently working up to being able to launch from 100,000 ft.
  • Re:Unit conversions (Score:3, Informative)

    by marm ( 144733 ) on Friday October 05, 2001 @03:11AM (#2391164)

    The whole idea of metric is that we should put all of our eggs in the one basket, so that people with certian brain defects would not be able to understand it. I found little logical in it to understand what people see so wonderful in it, and I have studied it for thirty years now.

    Umm, no. The beauty of metric, or rather the more modern form of metric called SI (Systeme Internationale) is that:

    a) multiples of a unit are always in base 10, so it is obvious that 27km = 27000m, and it is just as simple to write that in scientific notation (i.e. 27km = 2.7x10^4m) - you try telling me what 27 miles is in feet without reaching for a calculator

    and b) there is a small set of measured base units (there are 7 - metres, kilograms, seconds, amperes, kelvins, moles and candelas) and every other unit used throughout science and engineering is directly derived from these base units without any fudging

    Quite apart from the obvious benefits for calculation, it also makes things much easier to understand in your head - you only need to know the size of the 7 base units to be able to have some idea of exactly what each derived unit means. Also, if you are sticking to SI notation to the letter, it is plain from the name of the derived unit exactly how it is derived from the base units.

    Really, it is perfectly logical, and a heck of a lot simpler to learn than the old Imperial or Imperial-derived systems, where there were about 3 times as many different base units. Science has adopted SI worldwide, partly for its ease and simplicity, and yes, partly because scientists want to be able to understand each other. In most countries, engineers have also adopted the system for similar reasons, and even the general populace understands most of it thanks to everyday things being measured in SI units or multiples of - masses in grams or kilograms, volume in litres, distances in metres or kilometres.

    Anyway, in SI Units...

    160 knots = 82 ms^-1 (metres per second)
    6200 ft = 1900 m (yes, this one was right :)
    400 lbf = 1800mkgs^-2 (meters per kilogram per second, aka newtons)

    All conversions rounded to 2 significant figures... now, who's going to be the first to complain about the use of significant figures? ;)

  • by ruszka ( 456169 ) on Friday October 05, 2001 @03:22AM (#2391180)
    Not sure if it's been posted yet, but a guy out in Oregon is also working on something related to this.. Goes by RocketGuy [rocketguy.com]

    Everything he's worked on and gone through is pretty damn interesting, worth the read if you haven't heard of him.. He's set to launch in May of next year
  • by mks113 ( 208282 ) <{mks} {at} {kijabe.org}> on Friday October 05, 2001 @07:56AM (#2391458) Homepage Journal
    Looks like they are building five of them and plan to fly one this year. http://www.stormbirds.com/project/ [stormbirds.com]
  • Wrong! (Score:2, Informative)

    by archibald tuttle ( 456301 ) on Friday October 05, 2001 @10:40AM (#2392025)
    I do not know what kind of efficiency you mean, but in terms of energy efficiency rockets are actually very good. A rocket engine transforms about 90% of the chemical energy of the propellants to kinetic energy. This is excellent.

    The total energy efficiency of an orbital rocket can be defined as the potential energy of the empty rocket in orbit divided by the chemical energy in the propellants. Even here rockets are not that bad.

    If you have a hydrogen powered rocket with a specific impulse of 4300m/s and a total delta-v of 9000m/s, your mass ratio is 8.109, so the propellant weighs 7.109 times as much as the empty rocket. But the empty rocket has a specific kinetic energy of about 30 MJ/kg, whereas the propellants only have a specific chemical energy of 11MJ/kg. The total efficiency is thus 30/(7.109*11)=0.38. Not too bad, eh?

    The reason rockets are still so expensive is that most current rockets are direct descendants of ballistic missiles where cost was not important. And the shuttle is a f***ing joke.

    regards,

    tuttle
  • Re:Pointless (Score:5, Informative)

    by Rogerborg ( 306625 ) on Friday October 05, 2001 @11:26AM (#2392199) Homepage
    • Rockets are the most inefficient method of propulsion that's still in use, a better goal would be figuring out an entirely new propulsion system that could apply to everything

    Got any ideas? Once you're at the edge of the atmosphere, you're pretty much limited to using a self contained reaction motor.

    Ground laser launching relies on superheating air, plus it's only been used to shove vehicles directly up, so it's basically a really cool but expensive way to replace July 4 bottle rockets. A more viable alternative is turning beamed EM into electricity then powering magnetohydrodynamic motors that superheat air, but you still have that pesky problem that you are relying on an atmosphere to get your speed.

    You could accelerate the vehicle in a rail gun or rocket sled until it reaches orbital velocity while it's still on the ground. Ballpark figure, at a (barely) survivable 20g, you'd need a 150km track to reach the 7.73km/s orbital velocity of a typical shuttle mission, ignoring air resistance. Except you can't ignore air resistance, because at 7.73km/sec at 1 atmosphere, you'd burn the vehicle to a toasty crisp.

    Even if you postulated antigrav, you still need to generate lateral acceleration to achieve orbital velocity, which again requires a self contained rocket, or an atmosphere.

    A beanstalk (space elevator)? Heck, maybe we've already got the technology to do it, but we're not going to, not for a long, long time.

    So, really, if you've got any ideas about what to use as an alternative to rocketry today, let's hear them. I'm fresh out.

  • Re:Pointless (Score:2, Informative)

    by Oggust ( 526634 ) <d3august@dtek.chalmers.se> on Friday October 05, 2001 @11:39AM (#2392264) Homepage
    No, actually a ramjet is way more efficient than a rocket. A really good rocket motor gets an Isp of just over 400. (A little more if you feel like using F2 or ClF5 or other really nasty stuff, but nothing that dramatic.) A ramjet gets around 3000. It's a lot simpler than the rocket, and it doesn't have to carry it's own oxisizer, so it stands to reason. On the other hand, it doesn't work in space, and it needs to move a a pretty good speed before it starts working at all. /August.
  • Re:Rocket Racing! (Score:3, Informative)

    by John Carmack ( 101025 ) on Friday October 05, 2001 @02:58PM (#2393182)
    The rockets we are currently firing use hydrogen peroxide, which produces nothing but water and oxygen in the exhaust. Not even the most rabid greenie could argue with that.

    Hydrogen / oxygen rockets also produce water and excess hydrogen. Alcohol / ocygen rockets leave a few other things similar to auto exhaust, but not really worse.

    Solid rockets leave some bad stuff, and some propellants are truly nasty, like nitrogen tetroxide and hydrazine, but those are also much more expensive, so wouldn't be used in a cost effective program.

    John Carmack
  • Re:Pointless (Score:3, Informative)

    by Catbeller ( 118204 ) on Friday October 05, 2001 @03:56PM (#2393427) Homepage
    The "rocket sled" (actually a linear induction motor used as a railgun of sorts, also called a mass driver by Gerry O'Neill and company, and first dubbed a "catapult" by Heinlein and something totally else by Clarke) doesn't have to accelerate the ship to orbital speed. That's ludicrous.

    It merely has to replace the first stage, and that only requires a few miles of track, an upwardly sloping mountainside, and a few G's of acceleration. One the ship leaves the mouth of the catapult, it's moving fast enough for a very small fuel tank to kick it all the way to orbit -- not to mention the fact that at mountain height, it's past a goodly chuck of the atmosphere pretty quickly.

    It's surprising how little ship you need to achieve orbit once you get rid of the first few miles and get some speed buildup. The ship is SMALL.

    A catpult would prolly use maglev, be pretty cheap once the thing is built, and only require electricity to operate instead of rocket fuel. And it is reusable to a ridiculous degree.

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