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19 Apr 2024, 04:45 [ UTC - 5; DST ]


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 13:49 
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While we're talking impossible math, what about that kit cost of $130,000? Five seats, 300 kts, and pressurization for the price of a Carbon Cub!

Some of us will eat crow about this. I sincerely hope I'm one.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 13:51 
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Username Protected wrote:
All of the available HP to meet the performance claims isn't going to the propulsion. You still have to pressurize the plane, provide A/C, power deice or some way to pop boots, generate electricity and liquid cooling all under 3600 lbs.

The problem with this entire dream is that it's not based on innovation or new technology. It's was put together making the assumption that you could achieve twice the performance, half the weight, 3 times the range, four times the efficiency and do it all for 20 percent of the cost of anything else on the planet.


2000lb empty to create an pressurized airframe capable of dealing with 300knot true airspeed sure does sound like a pipe dream but it's almost been done before. Lancair IV-Ps came in at around 2200lb empty and many were capable of exceeding 300knots at altitude and stalled right below 70knots. They also didn't have 62" wide cabin and had flaps and I've never heard of one being built under $500K by the time all was said and done adjusted for today's dollars. So I agree that this is vapor ware even at 3x $130K.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 13:52 
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Username Protected wrote:
No, I don't believe the aircraft will cruise anywhere near 300KTAS, but even Mr. Mueller's math targets 230KT.

Maybe, still a big stretch.

The real problem here is not the original claims were wrong, the real problem is that the original claims exposed a fundamental and seemingly pervasive incompetence.

Start up aircraft projects like this fail all the time with competent engineering. They have no chance without it.

The only question left to answer is how long before the project dies.

For reference, consider a Lancair IV-P with 350 HP TSIO-550. 220 KTAS, 1347 nm range. That's what competent engineers can do. If someone claims they can be 10% faster with 20% more range than that on less power, be skeptical.

Mike C.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 13:55 
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Username Protected wrote:
No, I don't believe the aircraft will cruise anywhere near 300KTAS, but even Mr. Mueller's math targets 230KT.

Maybe, still a big stretch.

The real problem here is not the original claims were wrong, the real problem is that the original claims exposed a fundamental and seemingly pervasive incompetence.

Start up aircraft projects like this fail all the time with competent engineering. They have no chance without it.

The only question left to answer is how long before the project dies.

For reference, consider a Lancair IV-P with 350 HP TSIO-550. 220 KTAS, 1347 nm range. That's what competent engineers can do. If someone claims they can be 10% faster with 20% more range than that on less power, be skeptical.

Mike C.


Lancair IV-P with 350HP is not a 220knot aircraft. It will easily exceed 300knots at FL250. Not for long, but it will do it. It will cruise at 270knots all day long.

Last edited on 14 Dec 2017, 14:04, edited 1 time in total.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:03 
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Username Protected wrote:
For the prop efficiency conversation, note that the prop used on the Raptor is a 4-bladed MT running at a slower prop speed, which should be fairly efficient at altitude, however I haven't researched the actual MT data...yet.

The prop they are currently testing with the prototype is an MTV-14-D-C / CLD-190-17
http://www.mt-propeller.com/pdf/TCDS_EASA(Europe)/MTV-14_Issue1.pdf


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:07 
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Username Protected wrote:
Cirrus as a startup ... they did the same thing.
No they didn't, Cirrus hired competent engineers who knew and used the correct formulas.
Quote:
where will you be if they succeed?
This is engineering, not saving Tinkerbelle; whether we believe or not won't affect the outcome.

As I and others have said, I'd love to be proved wrong and for this to turn out well but the numbers, both in physics and finance, just aren't there for it to be possible. The only real question left is whether Peter is fooling himself along with his creditors.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:16 
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Username Protected wrote:
While we're talking impossible math, what about that kit cost of $130,000? Five seats, 300 kts, and pressurization for the price of a Carbon Cub!

Some of us will eat crow about this. I sincerely hope I'm one.


Let's not confuse "certified" with "experimental". You're buying a kit, not a turn-key airplane. Costs are a lot different when you're doing it yourself. I keep reading that it should cost more, but the reality is that you, the builder, need to contribute many hours of labor - and time is money. Let's assume 1500 hours of additional labor; go ahead and put a dollar to that.

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Last edited on 14 Dec 2017, 14:17, edited 1 time in total.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:16 
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Username Protected wrote:
Lancair IV-P with 350HP is not a 220knot aircraft.

Numbers came from Lancair's web site. You'd better tell them to fix it. :-)

The 300 knots number came from the turboprop version.

Quote:
It will easily exceed 300knots at FL250.

On a TSIO-550? In level flight?

Show me.

Mike C.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:22 
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Username Protected wrote:
You're inferring that Raptor engineers are incompetent; do you know that factually, or are you just speculating?

All the hard evidence suggests fundamental incompetence. For example, the claimed performance numbers.

If they can't compute some pretty basic performance numbers, what do you expect will happen when they come to modeling the spar strength?

People who pay these guys some money are victims, not customers.

Mike C.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:24 
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Username Protected wrote:

Let's not confuse "certified" with "experimental". You're buying a kit, not a turn-key airplane. Costs are a lot different when you're doing it yourself. I keep reading that it should cost more, but the reality is that you, the builder, need to contribute many hours of labor - and time is money. Let's assume 1500 hours of additional labor; go ahead and put a dollar to that.

I’m talking about a Carbon Cub kit.
And on the subject of kits, no one has ever built a Lancair IV-P in anything like 1500 hours or twice that.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:24 
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Username Protected wrote:
Finally set up for cruise at 75-percent power, the IV-P chugged right up to 195 knots indicated, for 278 knots true, or Mach 0.46, if you care to count it that way. This particular Continental, a longer stroke version of the Malibu engine, runs cleanly and smoothly lean of peak turbine inlet temperature; set 50 degrees lean, the fuel flow came down to 18 gph on the fuel flow computer.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:30 
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Finally, we'll get so see whether the left brain, or the right brain is better!

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:34 
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Username Protected wrote:
Lancair IV-P with 350HP is not a 220knot aircraft.

Numbers came from Lancair's web site. You'd better tell them to fix it. :-)

The 300 knots number came from the turboprop version.

Quote:
It will easily exceed 300knots at FL250.

On a TSIO-550? In level flight?

Show me.

Mike C.


I'm not sure what website you're referring to. If it's the new web site, they have pretty much all the information wrong. If IV-P only cruised at 220knots, there would no reason for it to exist. That's Mooney Bravo territory. Mooney Acclaim will hit 240 at FL250 and cruise around 230.

http://www.lancairowners.com/wp-content ... airIVP.pdf

.53Mach at FL240

It is one sleek airframe. 270knots all day long.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:46 
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Location: phoenix, AZ (KDVT)
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Username Protected wrote:
While we're talking impossible math, what about that kit cost of $130,000? Five seats, 300 kts, and pressurization for the price of a Carbon Cub!

Some of us will eat crow about this. I sincerely hope I'm one.


Let's not confuse "certified" with "experimental". You're buying a kit, not a turn-key airplane. Costs are a lot different when you're doing it yourself. I keep reading that it should cost more, but the reality is that you, the builder, need to contribute many hours of labor - and time is money. Let's assume 1500 hours of additional labor; go ahead and put a dollar to that.[/quote]

The Raptor website says you'll spend 2 or 3 weeks at their build center to fulfill the 51% rule. This is not 1500 hours additional labor.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 14 Dec 2017, 14:50 
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It also isn’t possible for $130k.


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