I think the stall speed you propose would be very difficult to achieve. The current wing area spec is a bit optimistic. And includes the fuselage, which is a little bit of a stretch for 100% effectiveness.
Ron Freiberger mailto: rfreiber...@swfla.rr.com -----Original Message----- From: krnet-bounces+rfreiberger=swfla.rr....@mylist.net [mailto:krnet-bounces+rfreiberger=swfla.rr....@mylist.net] On Behalf Of Architectural Engineering LTD Sent: Thursday, February 13, 2003 4:08 PM To: kr...@mylist.net Subject: KR>Building a KR2(S) as a UK microlight. Hi, Does anyone know if a KR2 or a KR2S could be built within the CAA's microlight definition (basically MAUW 450Kg or less (990lb) and [a stall speed of 32 Statute mph] or [a max wing loading of 25Kg/m2 ( 5.11lb/ft2)]? Changing to a smaller or 2-stroke engine would be OK. Cheers, Tim Walker. --- Outgoing mail is certified Virus Free. Checked by AVG anti-virus system (http://www.grisoft.com). Version: 6.0.489 / Virus Database: 288 - Release Date: 10/06/2003 _______________________________________________ see KRnet list details at http://www.krnet.org/instructions.html
