X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 30 Dec 2005 23:14:40 -0500 Message-ID: X-Original-Return-Path: Received: from smtp113.sbc.mail.mud.yahoo.com ([68.142.198.212] verified) by logan.com (CommuniGate Pro SMTP 5.0.5) with SMTP id 906533 for lml@lancaironline.net; Fri, 30 Dec 2005 16:32:43 -0500 Received-SPF: none receiver=logan.com; client-ip=68.142.198.212; envelope-from=elippse@sbcglobal.net Received: (qmail 23007 invoked from network); 30 Dec 2005 21:31:59 -0000 Received: from unknown (HELO Computerroom) (elippse@sbcglobal.net@66.122.72.85 with login) by smtp113.sbc.mail.mud.yahoo.com with SMTP; 30 Dec 2005 21:31:58 -0000 X-Original-Message-ID: <00b201c60d88$77289720$55487a42@Computerroom> From: "Paul Lipps" X-Original-To: Subject: Fw: lml_Web_Archive X-Original-Date: Fri, 30 Dec 2005 13:31:57 -0800 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_00AF_01C60D45.68207560" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.2180 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 This is a multi-part message in MIME format. ------=_NextPart_000_00AF_01C60D45.68207560 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Hi,all! I know this isn't e-bay, but I know the exact formula for the timing = of Klaus' PLASMA I,II,III NA, HC, and Turbo! What am I bid? In a chemically-correct mixture, it only requires 0.5 milli-Joule to = obtain ignition. PLASMA's put out in excess of 120mJ. PLASMA l&III have multiple, opposite polarity sparks that really excite = the molecules in the intervening gases which then get very hot, hence = the name PLASMA. Notice: this spark is a very light violet color, almost = transparent rather than blue, and a piece of paper put in the gap will = ignite! In all this discussion of timing and thetaPP, no one has mentioned = flame-front propagation speed vs charge density. Litton Industries and Hughes had D-Sub connectors on their approved list = for spacecraft. 'Course, gold only, not tinned! Now for a request. I fly a 235 with an O-235, 9.7:1 CR, putting out = about 123 SL hp at 2800 rpm, with dual PLASMA I ignitions and an ELIPPSE = three-blade prop with 76" effective pitch. I have extended wing tips = which add about 2 sq. ft. and 20" span. I get 1550 ft/min ROC at SL, = 2420 rpm, 110mph IAS, 1350 lb. At 1000' dalt, 2950 rpm I get 214 mph = TAS; at 10,000' dalt, 2800 rpm, I get 201 mph TAS, and at 14,500' dalt, = 2750 rpm, I get 198 mph TAS at 5.8 gph. These numbers were all obtained = with a highly-calibrated pitot-static system, true OAT, and a GPS. I = would like to get comparative data from those of you who fly 235's. = Thanks! Paul ------=_NextPart_000_00AF_01C60D45.68207560 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

Hi,all!

I know this isn't e-bay, but = I know the=20 exact formula for the timing of Klaus' PLASMA I,II,III NA, HC, and = Turbo! What=20 am I bid?

In a chemically-correct mixture, it only = requires 0.5=20 milli-Joule to obtain ignition. PLASMA's put out in excess of=20 120mJ.

PLASMA l&III have multiple, opposite = polarity sparks=20 that really excite the molecules in the intervening gases which=20 then get very hot, hence the name PLASMA. Notice: this spark = is a very=20 light violet color, almost transparent rather than blue, and a = piece of=20 paper put in the gap will ignite!

In all this discussion of timing and thetaPP, no = one=20 has mentioned flame-front propagation speed vs charge = density.

Litton Industries and Hughes had D-Sub connectors on their approved list for spacecraft. = 'Course,=20 gold only, not tinned!

Now for a request. I fly a = 235 with an=20 O-235, 9.7:1 CR, putting out about 123 SL hp at 2800 rpm, with dual = PLASMA I=20 ignitions and an ELIPPSE three-blade prop with 76" effective pitch. I = have=20 extended wing tips which add about 2 sq. ft. and 20" span. I get 1550 = ft/min ROC=20 at SL, 2420 rpm, 110mph IAS, 1350 lb. At 1000' dalt, 2950 rpm I get = 214 mph=20 TAS; at 10,000' dalt, 2800 rpm, I get 201 mph TAS, and at 14,500' dalt, = 2750=20 rpm, I get 198 mph TAS at 5.8 gph. These numbers were all obtained with = a=20 highly-calibrated pitot-static system, true OAT, and a GPS. I would = like to=20 get comparative data from those of you who fly 235's. = Thanks! =20 Paul

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