JetZero. Another Hobby Shop Using Other People’s Money

X3 Skier

Final Approach
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This one is a little more realistic than Boom but I predict they will finish second in the race to Bankruptcy to Boom.

Check out the picture of the Pickup Truck. Cheap Low Speed Wind Tunnel?

They did get into the fantasy section of the Wall Street Journal.

Wonder how the engines will like the boundary layer air ingestion on rotation.
 
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People around here are pretty excited. They are building a $4+ Billion facility at the KGSO footprint in Greensboro, NC, joining HondaJet, some smaller companies, and the Guildford County Community College aviation program. There's some planned program coordination with GCCC and some 14,000 jobs are promised. Groundbreaking scheduled for early 2026.

Promises are easy; delivery more difficult. We'll see.
 
People around here are pretty excited. They are building a $4+ Billion facility at the KGSO footprint in Greensboro, NC, joining HondaJet, some smaller companies, and the Guildford County Community College aviation program. There's some planned program coordination with GCCC and some 14,000 jobs are promised. Groundbreaking scheduled for early 2026.
I'll take the under.
 
People around here are pretty excited. They are building a $4+ Billion facility at the KGSO footprint in Greensboro, NC, joining HondaJet, some smaller companies, and the Guildford County Community College aviation program. There's some planned program coordination with GCCC and some 14,000 jobs are promised. Groundbreaking scheduled for early 2026.

Promises are easy; delivery more difficult. We'll see.
Hopefully it works out. At a minimum hopefully it creates some jobs for the community (and I like that they're partnering with a community college). At a minimum hopefully the kids from that program get some valuable experience.

But I admit, I'm always a bit weary of companies that drop hundreds of millions of billions on PP&E before they have a functional product.
 
Just saw the write up in Flying about United jumping in.

It just looks like the ALICE issue all over again. Do a pretty artist rendering and make money. And like the ALICE there appears to the eye several issues of aerodynamics. Rudder area looks like the styling got the better of the aerodynamic department. And the surfaces are very close to the CG point. Pitch control looks non-existent at slow speed and high angle of attack with fuselage blanketing the airflow. No flaps on the wing TE. No passenger windows aft of the wing, so the CG is going to be interesting putting passengers in when the majority are forward of the CG. A canard would at least make it look flyable. And the size of the cockpit windows and the location of and size of passenger cabin make it look like Munchkins will be riding the baggage compartments. And how will those engines work with ice coming off the fuselage or the airflow changes on take off and landing vs. cruise with all the area and local airflow in front of the intakes. There is a reason engines are put on pylons.

Wish that these vaporware airplane artists would at least make the plane look flyable. Or at least learn the ALICE story of money is easy to attract from non-pilots and disappears even easier. And that a letter of intent isn't the same as dollars in the bank.

Or maybe they did learn the ALICE story and take the money and run could be done better. . .Any plane that promises "to reduce fuel burn by as much as 50 percent per passenger mile" is a scam. If that were true, Boeing and AirBus would be flying that already. Do they know how hard it is to even get 5% with the laws of physics and aerodynamics and still keep it controllable in all flight ops?

1768434728322.png
 
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I've seen pictures of various craft with equal chances of flying in 1950s era Popular Mechanics. And sci-fi pulp novels.
 
And like the ALICE there appears to the eye several issues of aerodynamics. Rudder area looks like the styling got the better of the aerodynamic department. And the surfaces are very close to the CG point. Pitch control looks non-existent at slow speed and high angle of attack with fuselage blanketing the airflow. [...] A canard would at least make it look flyable. [...] And how will those engines work with ice coming off the fuselage or the airflow changes on take off and landing vs. cruise with all the area and local airflow in front of the intakes. There is a reason engines are put on pylons.
Yeah, the configuration is completely unworkable from an integrated aerodynamics and propulsion standpoint...right? Completely uncontrollable and unflyable...right? Non-existent pitch control at high alpha makes it impossible to recover from stalls...right?

Rebuttals of the above aero-propulsion "assessments" with the exception of ice ingestion were successfully demonstrated in flight from 2007-2013 (non-continuous).

X-48B:
ED07-0164-05~large.jpg


X-48C:
741109main2_ED13-0057-41_672.jpg

photo credits: NASA

Nauga,
in the papers
 
I spent some time reminiscing about the X-48 program today after learning that Bob Liebeck, the "father of the blended wing-body" and a friend and mentor, passed away yesterday. Funny to see this thread again. :confused:

Nauga,
dammit
 
I've seen pictures of various craft with equal chances of flying in 1950s era Popular Mechanics. And sci-fi pulp novels.
Why doesn't the B-2 fly? Or the B-49?

No passenger windows aft of the wing...
There would be few window seats for this design, renderings for this sort of plane in the past show seating similar to a theater. Lots of middle seats- I think there will be flying customer pushback from this more than anything else. The windows depicted are probably for first class pax.

I'm not saying JetZero will make a viable product- I'm in agreement that it likely won't come to anything. Bringing a design to market costs a lot of money, and proving a radical design will take more money.
 
Yeah, the configuration is completely unworkable from an integrated aerodynamics and propulsion standpoint...right? Completely uncontrollable and unflyable...right? Non-existent pitch control at high alpha makes it impossible to recover from stalls...right?

Rebuttals of the above aero-propulsion "assessments" with the exception of ice ingestion were successfully demonstrated in flight from 2007-2013 (non-continuous).

X-48B:

photo credits: NASA

Nauga,
in the papers
They did add a whole empennage to the later version. Was it for decoration or was it necessary to improve the flight characteristics? It took the whole BW tailless delta kinda concept and turned it into a BW tailed delta.

But yeah, these concepts have been around for a long time. My father used to bring home Lockheed's weekly (monthly?) newspaper and it had artists concepts like these (also WIG concepts) in the '70's.
 
They say they received an airworthiness certificate to fly the scaled model version almost 2 years ago, but I don't see any press releases of an actual test flight having taken place.
 
There would be few window seats for this design, renderings for this sort of plane in the past show seating similar to a theater. Lots of middle seats- I think there will be flying customer pushback from this more than anything else. The windows depicted are probably for first class pax.

We just need to give Junkers a call. They solved this back in the 1940s. Bring back passengers in wing roots with forward facing windows. Haha!

Bundesarchiv_Bild_146-1980-085-32,_Flugzeuge_Junkers_G-38.jpg
 
They did add a whole empennage to the later version. Was it for decoration or was it necessary to improve the flight characteristics?
There was (and still is) a lot of effort being put into noise reduction for large airplanes. The 3 engines were replaced with 2 high-ish bypass turbofans built around the same core as the original turbojets and the vertical stabilizers and associated rudders were moved inboard to shield the engines to reduce the noise signature. Both configurations used drag rudders on the outboard wings to supplement directional control power. There was no change in the number and style of directional stability and control effectors (i.e. stabilizers and rudders), and in the pitch axis the number of effectors (elevators and elevons) either stayed the same or was reduced by 2 (I can't recall which). The aft deck between the verticals was extended a bit to shield the exhaust signature below There was no empennage added and the changes were not made to address aerodynamics.

ETA: Before someone calls it out, the stinger out the back end is part of the AOA hangup/spin recovery parachute system (which was never fired in anger), and the two out front are air data probes with AOA and sideslip vanes.

Nauga,
out there
 
Why doesn't the B-2 fly? Or the B-49?


There would be few window seats for this design, renderings for this sort of plane in the past show seating similar to a theater. Lots of middle seats- I think there will be flying customer pushback from this more than anything else. The windows depicted are probably for first class pax.

I'm not saying JetZero will make a viable product- I'm in agreement that it likely won't come to anything. Bringing a design to market costs a lot of money, and proving a radical design will take more money.
I had the same thought but then I reflected that on all of my recent flights, people kept the window shades down (I didn't, I like to look) and used their devices. I don't think lack of window seats is a problem any more.
 
There would be few window seats for this design, renderings for this sort of plane in the past show seating similar to a theater. Lots of middle seats- I think there will be flying customer pushback from this more than anything else. The windows depicted are probably for first class pax.
I don't know how important windows are to passengers. I recently flew a ~1000nm commercial round-trip on 737s, outbound during daytime and return in the evening/early nighttime, and both flights appeared to have most of the window shades down the whole time, even for takeoff and landing. I don't fly commercial very often, so I don't know if this is typical.

Edit: Hah, @jsstevens and I had almost the same response at the same time.
 
I don't know how important windows are to passengers. I recently flew a ~1000nm commercial round-trip on 737s, outbound during daytime and return in the evening/early nighttime, and both flights appeared to have most of the window shades down the whole time, even for takeoff and landing. I don't fly commercial very often, so I don't know if this is typical.

Edit: Hah, @jsstevens and I had almost the same response at the same time.
Yes, and I have done a fair amount of commercial in the last 6 months. It's all the same. Shades down, devices on.
 
What if you fly on a 787 or 350 and the force darken it from the crew station with no passenger override option?

Then I just drink a lot, get in a fight with a flight attendant, go viral and get kicked off the plane, duh.
 
Passenger comfort and windows are one hurdle, airport infrastructure is another. All commercial airport terminal and gate space is designed around traditional tube style aircraft. Any blended wing would require reconfigured parking, gates, perhaps even taxiways depending on gear track and wingspan. That is where the A380 and some of other new planes struggle, airports just weren't designed with them in mind. Look at all the effort in the 777X folding wingtips.
 
I had the same thought but then I reflected that on all of my recent flights, people kept the window shades down (I didn't, I like to look) and used their devices. I don't think lack of window seats is a problem any more.
I don't know how important windows are to passengers. I recently flew a ~1000nm commercial round-trip on 737s, outbound during daytime and return in the evening/early nighttime, and both flights appeared to have most of the window shades down the whole time, even for takeoff and landing. I don't fly commercial very often, so I don't know if this is typical.

Edit: Hah, @jsstevens and I had almost the same response at the same time.
People use the side of the plane to rest against too. I think this is one of the arguments that United Airlines uses for their defense in the lawsuit that they sold "window seats" with no windows. I'll lean against the side of the plane for sleeping myself on long flights.

Theater seating also means many fewer aisle seats- it's bad enough now being #6 in an A380 in a 3-5-3 configuration (middle seat). Imagine the center seat being #11 from either side.
If I have a window seat, a window is important.
I prefer it too.
 
Theater seating also means many fewer aisle seats- it's bad enough now being #6 in an A380 in a 3-5-3 configuration (middle seat). Imagine the center seat being #11 from either side.
I expect emergency egress requirements would pretty much rule out having to crawl across 10 seats to get out in under 90 sec. There's no reason to expect a traditional 1- or 2-aisle seating configuration in a radically new airframe configuration.

Aside: No one's yet mentioned the ride quality considerations for someone sitting at the cabin walls, particularly when rolling in or out of turns. :cool:

Nauga,
floating but not clogging
 
I expect emergency egress requirements would pretty much rule out having to crawl across 10 seats to get out in under 90 sec. There's no reason to expect a traditional 1- or 2-aisle seating configuration in a radically new airframe configuration.

Aside: No one's yet mentioned the ride quality considerations for someone sitting at the cabin walls, particularly when rolling in out our of turns. :cool:

Nauga,
floating but not clogging
Good points. But they may make people crawl across 5 seats.
 
Good points. But they may make people crawl across 5 seats.
I'm curious about how you arrived at 5. Has anyone got an 11-across seat configuration now? It's not likely that the 90 sec requirement will change, and it really comes down to whether or not that can be met. I'm not aware of anyone with an 11 seat row now, and the egress requirement is already a tough one to meet.

Nauga,
and that Led Zepplin song
 
I'm curious about how you arrived at 5. Has anyone got an 11-across seat configuration now? It's not likely that the 90 sec requirement will change, and it really comes down to whether or not that can be met. I'm not aware of anyone with an 11 seat row now, and the egress requirement is already a tough one to meet.

Nauga,
and that Led Zepplin song
Two words…ejection seats. ;)
 
I'm curious about how you arrived at 5. Has anyone got an 11-across seat configuration now? It's not likely that the 90 sec requirement will change, and it really comes down to whether or not that can be met. I'm not aware of anyone with an 11 seat row now, and the egress requirement is already a tough one to meet.

Nauga,
and that Led Zepplin song
The A380 has 11 across, but with 2 aisles; the center section is 5 across (3-5-3). The number 5 was just a number I made up that seems reasonable. I'm convinced that the designers will maximize the number of pax in the plane. Even if there is only 5 across, there will be many more middle seats than there are now. Even with 3-3-3 configuration, middle seats are 1/3 the number of seats (approximately- some pedant will note exceptions). A 5-5-5 configuration will make ~2/3 the seats middle seats.

I thought about the 90 second evacuation time, but didn't the A380 wing fail at 3-4 % of the maximum it was supposed to, and yet get certificated? I'm cynical enough to believe that a campaign contribution to the right people can change the evacuation time requirement.
 
The A380 has 11 across...
We're talking about different things here. Longer continuous rows require more time to egress from middle seats than discontinuous rows with the same number of seats separated by aisle, this impacting egress time.

but didn't the A380 wing fail at 3-4 % of the maximum it was supposed to..
No. It initially failed at 5% *below* the limit it was required to reach. Still a failure, but hardly comparable; and irrelevant to egress time. Regardless, the wing structure was modified to comply with the requirement. The waiver you imply may have been for the requirement to physically demonstrate that compliance on the structural test rig but I'm not certain.

Can you find an airplane that's gotten a waiver on the egress time? I cannot, and I know manufacturers consider it a critical test.

Nauga,
and suitcases in the aisles
 
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We're talking about different things here. Longer continuous rows require more time to egress from middle seats than discontinuous rows with the same number of seats separated by aisle, this impacting egress time.
No, talking about the same things. I did specify the aisles in the part of the statement that you cut, thereby recognizing the egress time. Given what exists now, a row of 5 seats between aisles is certainly possible.

My comments were really about the increased number of "middle" seats this design would allow, which are less desirable than either window or aisle seats.

Both the Boeing (X-48) and Airbus (MAVERIC) designs have been flying (flown?) for some time. If those companies haven't made a lot of progress on blended wings, I doubt JetZero will. As a result, we both probably wasted more time on this discussion than we should have.
 
Yeah, the configuration is completely unworkable from an integrated aerodynamics and propulsion standpoint...right? Completely uncontrollable and unflyable...right? Non-existent pitch control at high alpha makes it impossible to recover from stalls...right?

Rebuttals of the above aero-propulsion "assessments" with the exception of ice ingestion were successfully demonstrated in flight from 2007-2013 (non-continuous).

X-48B:
ED07-0164-05~large.jpg


X-48C:
741109main2_ED13-0057-41_672.jpg

photo credits: NASA

Nauga,
in the papers

I note that they have rudders, the C has engines above the fuselage. Not the artist's idea above. . . The B-2 and other flying wings have a different mission and risk assessment. I'll trust those engineers long before an upstart company with a painting. Just look at how much money ALICE burned through with a new design. . . They started up at Arlington for a test flight, that didn't work, too many cameras, one guesses. Even after a very short test flight at MWH, some of us knew the suspicions were correct. Hardly any postflight details, the flight was to keep the money flowing. The shortness of the flight said they had issues, and the test pilots were pretty tight-lipped. A few more years, no photos of any version 3 released as they built it, but more paintings. Well, it was then obvious. Clickbait for private equity firms wanting to waste money. And yes, the expense of a FAA certified factory made the prototype work peanuts. What is new in aviation is just a replay of the decades before. Just read 1950 Popular Science articles. Just a little more gloss and computers. But the air doesn't care and aerodynamics are the same. IMHO.
 
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Just reread the propaganda and looking forward to the first full scale flight in “2027”. My view is that’s like the Joe’s Crab Shack sign. “ Free Crabs tomorrow “.

Maybe it’s a 3D printed test plane since they haven’t shown ANY hardware.

Sort of like when the A-12 program promised first flight in two years when all they had were paint stripes where the jigs would go after they were designed and built.
 
This one seems to have serious investment, both from the government (Air Force) and the private sector (United, Alaska and VCs), so it will likely be around for a while. The scale model Pathfinder has flown and data from that work is going into construction of the full scale demonstrator at Scaled Composites. I don't travel much anymore, so I'll watch as a mildly interested bystander. It would seem to need considerable changes at airports to facilitate loading and unloading passengers. That may be as big a hurdle as all the issues raised about aerodynamics. I also worry a bit about pressurization of the cabin. The tubular shape of current airliners is easy to design for pressurization loads, but the modeling and construction to address pressurization stresses for a blended wing body will be much more complicated. Still, I think it is fun to see new ideas developed and tested. The lack of windows could easily be addressed with little cameras feeding one or more channels on the entertainment screens. Just as watching football on TV gives me a better view of the game than any seat in the stadium, cameras could offer passengers more, and better views than window seats offer. And every passenger would then have a "view seat".
 
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