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
  #4  
Old September 30th 03, 09:42 PM
Dan DeLong
external usenet poster
 
Posts: n/a
Default


My O-320 powered Long EZ doesn't climb at 10,000 fpm at Vne.

Actually, Rick, the web site says, "Single engine performance is
similar to a Lycoming O-320 with constant speed prop." So in that
statement they are talking about performance with only one of the two
rockets firing. 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
 




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 09:25 AM.


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