A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Home Built
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

question about EZRocket



 
 
Thread Tools Display Modes
Prev Previous Post   Next Post Next
  #5  
Old October 1st 03, 06:38 AM
David O
external usenet poster
 
Posts: n/a
Default

(Dan DeLong) wrote:

Even so, the statement is not entirely accurate.

David O --
http://www.AirplaneZone.com


As Dave Barry would say, "an alert reader....".... You are correct in
your observation. The more complex and more correct statement is that
the single engine ground roll and takeoff are similar to an O-320 with
constant speed prop at a low MSL airport. After takeoff, the piston
engine/prop thrust drops with indicated speed whereas the rocket
engines have constant thrust. Also, the piston engine power drops with
altitude.

And the reason for the short airshow routine was because the events
coordinator asked us to keep it short. Otherwise, Dick would have done
a second go-around (which he practiced at Mojave the week before). We
landed with about half of the propellants remaining, which was why we
did the LOX vent after landing and before rolling into the crowd. Too
bad; that second go-around is more impressive at lighter weight.

Glide and landing are similar to a standard Long, except that the
rocket has less drag (the added fuel tank has less drag than the prop
and cooling drag did), and the belly board is less effective ahead of
the fuel tank.

Dan DeLong
XCOR Aerospace


Yes, Dan, I ran the numbers for a flat 400 pound thrust using the drag
curve of my Long EZ at 1200 lb. Best rate of climb was 2,770 fpm at
130 kt. That's why I concluded, "not entirely accurate". I then ran
the numbers for both engines firing and got a best rate of climb of
8,100 fpm at 185 kt with an aircraft weight of 1200 lb.

As for the LOX vent at Oshkosh 2002, that was something to see. I
think it was you I questioned afterward and you said it really was not
dangerous without some sort of fuel to burn. You (or whomever) said
you had once purposely put a lit cigarette into the O2 cloud -- the
cigarette burned quite rapidly and that was the extent of the effect.

Thanks putting the videos on your XCOR web site. Riding along with
Dick was a trip. I could hear the concern in his voice on that early
run when the engine didn't shut off as commanded, "We've got a major
problem here."

David O -- http://www.AirplaneZone.com


 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
Tailwheel question Steve B Aerobatics 4 January 30th 04 04:35 AM
Air compressor question Frederick Wilson Home Built 40 October 6th 03 03:50 AM
Question on Pulsejets/Ramjets??? DarylG1532 Home Built 3 August 16th 03 04:20 AM
AVID FLYER question OB1 Kanobe Home Built 0 August 14th 03 03:46 PM
question on intercoms for my new homebuilt w b evans Home Built 1 July 23rd 03 01:57 AM


All times are GMT +1. The time now is 12:32 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.