Re: turbine engine with thrust to weight ratio less than one to one?
- From: "Michael Nouak" <nospam@xxxxxxxxxxxx>
- Date: Thu, 1 Sep 2005 14:12:17 +0200
Any APU should fit the bill. The Hamilton Sundstrand APS 3200 installed on
Airbus A320 series a/c weighs 140 kgs and produces 124 SHP. The thrust
produced by the exhaust should be rather negligible.
http://www.hs-powersystems.com/products/aps3200pds.htm
HTH,
Mike
"scupper79" <scupper79@xxxxxxx> schrieb im Newsbeitrag
news:1125554892.b533f98d63a2fcea442400dcdaa89a23@xxxxxxxxxxx
>
> I need a turbine engine with a thrust to weight ratio of less than one to
> one.
>
> This is a school project and is all just theoretical.
>
> thanks,
> ck
>
.
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