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#1
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what is their site?
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#2
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Kevin
Know about the two 'poles' that extend to stabilize the seat and establish a direction in the prevailing air direction. After ejection and stabilization some rockets fire to boost the seat to enough altitude for seat separation and chute to open prior to pilot hitting ground. Know that the Russian seat was looked at closely for the F-22 but someone (political) sold the idea of home grown vs imported. We have all seen the Russian seats work. Farnsboro/Paris Air Show. Worked fine (super to be exact). On air speed to eject. Air Force found out that going Mach 2 and losing an engine (or breaking up) you decelerate to under mach one almost immediately so that established their top design criteria for seats. When I ejected, it was at low speed and about 8K (over the ice cap in Greenland) above the ground with bird under control. Worked fine and didn't even get any crotch black and blue marksG Was in NORAD but never landed at Cold Lake. stationed at Bangor AFB, Maine for four years and we flew into and over eastern Canada on many missions. Great troops canuks. Have a nice day Big John Point of the sword On Mon, 30 Jun 2003 11:42:08 GMT, Kevin Horton wrote: In article , Big John wrote: Model Flyer 1. Ejecting at 800 mph on the ground has a few things to consider, both good and bad. 2. Current ejection seats are called 'zero zero' seats. This means they can be used sitting on the ground and with zero forward speed. 3. The initial 'push' to clear the vertical fin on their fuselage can be accomplished well within current technology. 4. Some of the bad things: a.Air Force found out that one of the problems with high speed ejections was 'flailing' of the arms (and legs). Of most importance was the arms with the joints receiving a lot of damage. For high speed ejections, I would want one of the Russian Zvezda K-36DM seats. Good to 1,400 km/hr equivalent airspeed (755 KEAS, 870 mph EAS). I was stationed at the Aerospace Engineering Test Establishment in Cold Lake, AB when the iron curtain came down. Our lead ejection seat specialist was at one of the first ejection conferences that had Soviet participation, and he spent some time talking with them. He was very impressed with how well their seats protected the crew. They had a much, much greater percentage of ejections that ended up with no injury to the crew than was seen with western seats. At the time, the western world was working on the 600 kt barrier (i.e. a seat design that allowed ejections with no injury at 600 kt). The Russians were working on the Mach 3 barrier. Their seats have telescopic stabilizing booms that provide drag to keep the seat facing into the wind. They have arm and leg restraints, and a blast shield that comes up between the occupant's legs and extends in front of the chest (sounds a bit scary if you are well hung). The only downside of the Russian seats is the weight - they were about twice as heavy as the western seats. The USAF is seriously considering a lightened version of the Russian seat for future aircraft. It looks like they removed the blast shield in this version, which lowers the max speed rating down to 700 kt. http://www.zvezda-npp.ru/english/05.htm http://users.bestweb.net/~kcoyne/k36seat.htm http://www.afrl.af.mil/successstorie...warfighter/02- he-11.pdf |
#3
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In article , Prglgw
wrote: what is their site? Whose site? It's pretty hard to figure out what you are talking about when you don't quote the relevant part of the post you are referring to. -- Kevin Horton - RV-8 Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ |
#4
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In article , Prglgw
wrote: I was refering to the original content of this topic, the F104 fuselage intended to break the land speed record. The "site" was spoken of 3 or 4 times, but no one mentioned what it was, as well I was not aware that any other site was mentioned in any of the subsequent posts, so anyone reading about this topic would probably know which site I was looking for. I now see this was apparently not clear, so : could someone please give me the url to the site about the F104 land speed attempt? OK http://www.landspeed.com/ -- Kevin Horton - RV-8 Ottawa, Canada http://go.phpwebhosting.com/~khorton/rv8/ |
#5
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On Thu, 26 Jun 2003 12:09:14 +0100, "Model Flyer"
wrote: "Richard Riley" wrote in message .. . On Fri, 20 Jun 2003 02:21:11 GMT, Dave Hyde wrote: The scary part about this group is that they have... "an ejection specialist who worked on NASA space missions, a jet engine mechanic, a computer technician, a former B-52 mechanic, an auto body specialist, a machinist and an engineer." I don't see any problem with using an onboard computer providing they don't use a Microsoft Operating System, windows hangs several times a day unless you just leave it alone. I'm currently running 4 machines, the slowest of which is a 1900 XP + Athlon with XP Pro. I haven't had a machine hang in months and these things run 24 X 7. Two of them are used for programming and two are used to photography. Storage is huge with the one in the shop running a tad over a half a terabyte while the others are close to 200 gig each. but no aerodynamosist. And I have to wonder about the inclusion of the ejection specialist. I guess if you have a seat already it might as well work, but there aren't many things that could go wrong with it that would both call for and allow ejection. The ejection seat is so the equipment can be saved if the thing goes out of control:-) silly remark, anyone any ideas on ejecting at 800+ at ground level? It would need a hair trigger and quite possibly eject the whole driver enclosure instead of just a seat. Unfortunately that didn't work well for the XB70 the only time it was needed. Roger Halstead (K8RI EN73 & ARRL Life Member) www.rogerhalstead.com N833R World's oldest Debonair? (S# CD-2) -- . |
#6
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In article , Roger says...
It would need a hair trigger and quite possibly eject the whole driver enclosure instead of just a seat. Unfortunately that didn't work well for the XB70 the only time it was needed. Similar rig in the B-58 worked alright. The one in the F-111 worked very well, and there are probably a couple 800 kt. ejections at nought feet in its history. I would agree with the poster (was it you?) that suggested an aerodynamicist might be a useful team member. cheers -=K=- Rule #1: Don't hit anything big. |
#7
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![]() "Big John" wrote in message ... Forget details now but didn't the capsule system crap out the first time it was used in a F-111? I think they had a fatal accident when the air bags didn't deploy. |
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