One of the more controversial aircraft ever deployed, the
Osprey has suffered years of criticism. Here is a short
report card with how the first batch of them are doing in Iraq.
The gist of it is, still controversial going by the reports.
"The engine was breaking up. Not a good thing. But
what's more interesting is the indication that the troubled
engine was still putting out considerable thrust, but the
aircraft couldn't maintain altitude," Bob Cox notes at
Sky Talk. " The V-22 is supposed to be able to fly at least
some distance and land on just one engine, but in this case it
was unable to hold altitude while still getting significant power
from the damaged engine. ed.z.: Has this plane ever been any
good? I just don't recall much about it other than people
thought it was an interesting idea, but the engineering left a
lot to be desired.
And now there is a new player in the field of short take off and
landing (STOL) load carriers. WhiteKnightTwo
can fly high enough to get above a lot of low tech anti aircraft
fire, and at low altitude it should be almost as manoevurable as
an Osprey.
My impression of the Osprey is that it is a critter that could
only have been designed by a committee of people with orthogonal
concerns that they were unwilling to compromise on.
Occasionally, such committees really do come up with very useful
results. However, they need to compromise a bit.
For example, what if instead of landing and taking off
vertically, we said we wanted this thing to land and take off on
very short, unimproved runways. Given 100' of runway
you could build some very useful troop transports that might be
able to fly pretty fast.
Those aircraft exist. Add a set of JATOs to them, and you
could get in and out of some very tight places. Ever seen
"Fat Albert" do a JATO takeoff in a Blue Angels
demo?
The problem is that the folks who insisted upon being able to do
vertical takeoffs and landings wouldn't consider the
alternative of very slow flight.
If anyone has ever seen the Itty Bitty Runway act at an air show,
it proves that with reasonable forward motion, you can put an
airplane down on a helicopter pad without a whole lot of
fuss.
Until the materials and engines improve (and there is hope that
they will), I think the Osprey will remain a dangerous aircraft
to fly.
As I understand it, it was specified to meet a tactical
requirement of the Marines. It had to be able to lift a $payload
from something similar to an LHD, fly
far and fast to an unimproved drop zone, deliver
its cargo on the ground, and take off to return. Furthermore it
should be able to cycle out to deliver a new load with nothing
more than a reload of cargo and fuel. Much of that requirement
that could be done with helicopters, but the problem with them I
think is both range (how far can they drop inland?) and speed
(how many drops can be made in an hour?). The ability to use
completely unimproved landing zones rules out anything but a VTOL
craft, while the quick sortie interval probably rules out any
kind of JATO-dependent craft.
It's a brutally difficult requirement from an engineering
perspective, but the Marines evidently are so firm in that
requirement that they've stuck with the Osprey for, what,
twenty years?
The V-22 Osprey is primarily a replacement for the CH-46 Sea
Knight, so STOL would be useless, VTOL is a hard
requirement. The Osprey can actually do STOL, and when it
does it can carry more payload, but VTOL is required for
shipboard operations, for dropping off and picking up troops in
remote locations - anywhere there is no airstrip, handling sling
loads, etc.
Using a tilt-rotor instead of a conventional helicopter provides
benefits in range and speed. The Marines want to be able to
get in and out of hot areas faster, helicopters are often lost in
transit as they fly low and relatively slow. The Osprey is
also slated for use in special operations and SAR, when being
able to transit fast is important, and you need to be able to
hover and land vertically when you get to the destination.
There do seem to be issues with the engines, and there is an
effort underway to address that. It may come down to
needing to replace the Allison AE-1107 engines with something
else if they can't correct the issues. But odds are
they'll get it worked out.
As for the issue of losing altitude with a busted engine, there
are important facts missing. What was the pressure
altitude? If they were flying in hot conditions and/or at
high altitude, both of which are likely in the region, then any
aircraft can be impacted by a loss of power. Was it in wing
borne or rotor borne flight when it happened? Rotor borne
is much more dependent on power. The Osprey can certainly
maintain altitude on one engine, that's been demonstrated,
but there are real world limitations - the higher the pressure
altitude the more power is required and the greater the impact of
any loss.
The V-22 is the first production tilt rotor, it should be
expected that it will experience issues as it breaks new
ground. The same things happened with the first jets, the
first helicopters, etc. There will be unexpected
engineering issues that come up, even with modern design tools.
You are using techno-babble to obfuscate the issue.
The Osprey was developed to solve problems with speed and
carrying capacity that the Air Cavalry (and similar groups)
encountered in VIETNAM.
In Veitnam, advances in helicopter technology allowed the
military to use a new type of engagement. They could use
helicopters to bring a large ammount of troops into an
inaccessable area in a short ammount of time, and theoretically
bring out the injured faster.
The PROBLEM was that there never seemed to be enough room on the
helicopters to take away all the wounded fast enough. Soldiers
had to watch their friends die in their hands because the
choppers were too slow or filled to capacity.
Those are the problems the Osprey was originally intended to
resolve. Straight line speed and capacity (with helicopter-level
VTOL ability).
Now, the boondoggle begins...
The problem is, and always has been that the two rotors can't
auto-rotate.
If one rotor fails, the damn thing flips over. At low altitudes
(where you're most likely to take fire from small arms that
could take out one of the rotors), the thing can't transform
to a plane fast enough to glide down. In one incedent, the thing
was doing a demonstration (that was supposed to show that it was
past it's problems and ready for deployment) in front of
Congressmen. An engine failed and it flipped, killing everyone
inside, including all the ace test pilots who had worked on
developing it for over a decade...all this
*in front of congressmen*
Just like any Military boondoggle, it's become a big session
of CYA (cover your ass). No one wants to admit that the thing
doesn't work AS INTENDED and doesn't solve the problems
it was supposed to solve.
Sure it can VTOL. Sure it's fast in straight line flight. But
it's never going to do what it was intended to do in it's
current incarnation. It's not approved for use in the heavy
combat situations it was originally intended for.
Boondoggle...50 Billion-plus down the drain so high up military
can save face.
It isn't technobabble, it is the accepted terminology.
And you're also incorrect. The crash 'in front of
congressmen' was due to a *fire* in a nacelle. It had
nothing to do with the ability to auto-rotate. If the rotor
hub in ANY helicopter burns, you're going to have a hard time
staying in the air. The Osprey can auto-rotate under normal
conditions - normal being the loss of an engine, not a nacelle on
fire. There is a shaft that connects the two nacelles that
allows one engine to power both rotors and keeps them in sync
even with loss of all power. I'll also note that the
crash in question was in 1992, very early in the life of the
Osprey, and it didn't involve 'flipping'.
Perhaps you're confused with the next incident listed, in
which the Osprey suffered a rotor stall during a steep simulated
combat approach and that resulted in a flip. But that was
due to vortex ring state, something which can happen to *all*
helicopters, not just the Osprey. And it only happened
because the crew exceeded the then permitted limits. They
broke the flight rules which were in place deliberately to help
prevent just that kind of accident. The Osprey's flight
control system was subsequently modified to help alert crews to
keep them out of the flight states where they may encounter a
vortex ring condition, but that's all you can do - it is
still possible to induce the problem, as it is in all
helicopters.
And you seem to ignore that the helicopter being replaced is the
CH-46 Sea Knight which is what? A tandom rotor
helicopter. And the US Army and USAF both use which
helicopter as their primary heavy lift helicopter? The
CH-47 Chinook, the Sea Knight's bigger brother - also tandem
rotor. The Osprey isn't so different from these
helicopters in practice. They both have their dual engines
in the tail, and use a long drive shaft to power the front
rotor. So there is experience with such power distribution
and gearing systems.
You lose one rotor on ANY tandem rotor helicopter and you're
in trouble. It happens to Chinooks and Sea Knights - loose
one and you flip. Period. It is like losing a wing on
a conventional aircraft. The Osprey at least has the option
of gliding if it happens with enough altitude, the -46/47 are
doomed any any altitude. On the -46/47 the rotors also
inter-mesh, and if they loose sync the rotors will destroy each
other, and that has happened - in fact it happened at an airshow
in front of major brass and the public, back in the 80s I
think. I can't be arsed to look up the date.
Conventional single-rotor helicopters also suffer fires,
transmission failures, tail rotor failures, etc. Does that
make them all boondoggles too?
And you refer to the conditions in Vietnam as if that makes your
point, but quite the contrary. The conditions in Iraq and
Afghanistan are, if anything, even more demanding than Vietnam,
with regard to air supply and medevac. The development of
MANPADS has increased the threat environment. And the
distances and terrain involved put a greater demand on rapid
ingress and egress, plus provide pretty much constant 'hot
and high' flight conditions which really tax aircraft,
especially helicopters. Being able to get in and out
quickly while still being able to VTOL is not something unique to
Vietnam which magically became unnecessary once that conflict was
over.
The V-22 is getting a lot of attention because it is new and
different. But if you look at the development of other
military aircraft you'll see that it is fairly common for
them to have development issues including the loss of airframes
during development and into their early service lives as they go
through their teething cycle. And this, unfortunately, has
often included the loss of life.
The tilt-rotor shows a lot of promise, and it is started to
deliver on those promises. The Osprey itself has gone
through several improvement cycles with modifications based on
experience in testing and deployment, and it will continue to do
so. The BA609 commercial tilt-rotor, which is based on the
experience developing the V-22 Osprey, is also now flying and
progressing nicely.
The Osprey is really the first of its kind. Its
predecessors were only research aircraft, such as the XV-15 (one
of the two of which also crashed when a bolt came loose in
flight, BTW), it is the first attempt at a production model of a
new type of aircraft. To not expect it to have some
teething issues would be unreasonable. And, unfortunately,
a number of the issues it has had are not at all endemic to the
design but rather are human error or carelessness such as
mis-wiring engine controls. That kind of mistake can, and
has, doomed any aircraft. They get more attention when it
happens on a special aircraft such as the Osprey.
As for not being approved for specific types of operation,
that's normal operating procedure for the first deployment of
any new system. You crawl before you walk before you run,
to build up confidence. Other current examples include the
initital combat deployments of the Dassault Rafale by the French,
and the initial deployments of the Eurofighter Typhoon.
When the C-130J first entered service it was kept to more of the
'milk run' missions until confidence and experience were
gained, and that was a derivative of a 50-year old design with a
proven record. So that argument is a red herring.
This is the first combat deployment of the Osprey, it would not
be a prudent risk to toss it in the deep end and hope everything
works as expected. Of course you would hope so, but many
plans and expectations wither when exposed to combat for the
first time. So you do it in phases and ramp up over time.
Well, obviously you know more about it than I do, tech-wise. I
appreciate your knowledge of the specifics, but I remain
unconvinced. I still see its existence as a 'boondoggle'
and here's why:
"Being able to get in and out quickly while still being
able to VTOL is not something unique to Vietnam"
That was never my point. I brought up 'nam to emphasize the
original intent of the aircraft and compare it to what has been
birthed...decades and billions of dollars later.
Specifically, you state that the V-22 is slated to replace the
twin-rotor CH-46 Sea Knight. That's its mission NOW. It was
originally intended for the Vietnam-inspired uses that I
described (and you tacitly acknowledge).
One of the main characteristics of a gov't boondoggle is all
the revisionist history necessary to turn the project into
something people can label as a 'success' and that's
what I see going on here. This is the crux of my argument.
Also,
"As for not being approved for specific types of
operation, that's normal operating procedure for the first
deployment of any new system. You crawl before you walk before
you run, to build up confidence"
Cop out...'crawling before you can walk' is one thing
(ex. mercury>gemini>apollo missions), but this beast
languished for decades, mired in the stench of government
mismanagement and CYA politicking.
Let's continue to use the apollo space missions as a
comparison. They allowed us walk on the moon and develop ICBM
capabilities for the cost of approx. $135 billion (in 2005
dollars, from wikipedia) *within 10 years* of the project's
inception.
The V-22 took over 20 years at the cost of $50 billion, and it
*still* isn't capable of fulfilling its original mission.
Now, I understand the time needed to develop new aircraft and the
sacrifices (fatal accidents included, unfourtunately). I respect
the people who develop new aircraft. But your argument that this
is 'typical development problems' is BS and a total cop
out.
Well, the bitch is here (v-22) and even Obama is tooling around
in it. For the record, I think it's cool. My point is that
'cool' does not cover the immense boondoggle of it's
development, and I disapprove of any revisionist history or
whitewashing to overlook that fact. We need to know what was done
wrong so we can avoid it in the future.
Just think: if military brass had been focused on delivering an
aircraft that completed the mission (as originally
envisioned...fast+VTOL+large capacity+heavy combat) instead of
myopically ramming the tilt-rotor design through the pipeline,
everything would have worked out better.
Anyway, thanks for the lively discussion. Again I appreciate your
deep tech. knowledge of the project.
I'm an aviation geek - I subscribe to Aviation Week for
enjoyment. :-) I studied Aerospace Engineering for the
first few years of college (in the early 90s) before I got sucked
into computing, which became my career. I've been
interested in the Osprey for a long time just because it is
interesting and different, and we don't see a lot of radical
change with new designs most of the time.
I agree that it has had an overly long development period, but a
lot of that has been due to hot and cold budgets. The
Osprey was nearly cancelled a few times and had its budget
slashed, and that really prolonged the development and raised the
costs dramatically. Perhaps we've ended up with a
better aircraft because of it, since there was more time to
revise the design and learn from mistakes, but perhaps we'd
already be on the V-22C model by now if it had gone into service
earlier. It is something we'll never know.
Specifically, you state that the V-22 is slated to replace the
twin-rotor CH-46 Sea Knight. That's its mission NOW. It was
originally intended for the Vietnam-inspired uses that I
described (and you tacitly acknowledge).
We're not really saying very different things - one of the
helicopters widely used by the Marines for that mission in
Vietnam? The CH-46 Sea Knight. So performing that mission has
always meant, in part, replacing the Sea Knight. Even
today, the Sea Knight is the helicopter the Marines still
primarily use for those missions. That's not really a
new goal for the Osprey. The Marines had hoped to have replaced
the Sea Knight years ago at this point, the airframes are very
old. And they stopped buying new models in anticipation of the
Osprey having been in service earlier. Performing those
Vietnam-inspired uses and replacing the Sea Knight are really the
same goal, since the Sea Knight is what they use for those
Vietnam-inspired uses today.
Other models the Marines used in Vietnam have largely been
retired already as the fleet has been simplified. The CH-53 is
still in service, but in the form of the new model CH-53E Super
Stallion. (And that's in the process of being evolved into an
even larger, heavier lift CH-53K model.) The CH-53E is almost an
all-new aircraft compared to the CH-53A-D models. Similarly
the Marines still fly the AH-1 Cobra, but today's AH-1W
SuperCobra and AH-1Z Viper are a far cry from the early models
used in Vietnam. I'd be surprised if they have any
components in common with the early models. Same goes for
the UH-1Y Venom which is only superficially similar to the
Huey's of Vietnam. The CH-46 is really the only
aircraft from the Vietnam era the Marines are still flying that
hasn't changed all that much. Not to say it is
identical or anything, but the last US airframes were built in
1971 - the war was still on in Vietnam when those airframes
rolled off the line. The US Navy retired all of their units
by 2004. The newest CH-46 airframes are 37 years old.
Sure, they've been upgraded in service a few times, most
recently in the 90s, but they're really wearing out.
I don't know what other design could really do what the
tilt-rotor does, and not be more complex. The
'X-wing' concept for stopped rotor flight would provide
the same basic features, but proved to be hugely complex and
expensive, far more than tilt-rotors, and was dropped.
Sikorsky is just now resuming work on the coaxial ABC (Advancing
Blade Concept) design, as they now feel the technology has
reached the point where it is feasible to make it work.
They tried it in the past, but ran into problems with the
materials and design tools of the day. Today's
composites and computing power give them a better shot. But
it is still a research effort, probably a decade away from
production possibilities.
Some argue that the tilt-wing is simpler than the tilt-rotor, but
it has issues in the transition from rotor-borne to wing-borne
flight (and vice-versa) as the wing is still at a very high angle
of attack while the rotors are losing vertical light in
transition. There are tilt-rotor concepts where the engines
remain horizontal while the rotors pivot through a gearbox.
It makes for a more complex gearbox, but simpler engine design
and mounting. But it is still a tilt-rotor in the end.
The problem with high speed flight in helicopters has always been
rotor stability. The advancing blade bites into the air
with the speed of the rotor *plus* the forward speed of the
aircraft, so it runs into compression shock before the
airframe. Meanwhile the retreating blade only bites with
the rotational speed *minus* the forward speed of the aircraft,
so it encounters aerodynamic stall earlier. And you get an
imbalance in lift well before that, of course. Modern
rigid, hingeless rotors and advanced blade designs (like the
British BERP rotor blades) have allowed helicopters to reach
speeds older models couldn't dream of, but they still
can't match fixed wing flight. Concepts like ABC show
promise, but much work remains to be done.
If we'd skipped the tilt-rotor and poured the same funding
into advanced helicopter designs, would we be closer?
Probably, sure. But from what I've seen in the
fundamentals, companies like Sikorsky, AugstaWestland, Bell, etc,
have never stopped doing R&D because there is commercial
demand and competition. And there have been fundamental
issues to overcome with materials, simulation, etc. So,
personally, I don't believe we'd have a deployable
helicopter with performance to match the Osprey by this point,
and probably not until next decade.
And given the even greater hurdles and costs than the Osprey,
such a program would have been more likely to be canceled - like
the RAH-66 Comanche. That program started out as the LHX
with broad goals of replacing the UH-1, OH-6, OH-58, and AH-1
with radical new technologies. And it was slashed
repeatedly until it was a much reduced partial replacement for
the OH-58 and AH-1, and then cancelled completely.
Instead the ARH-70 is replacing the OH-58D, and it is an
'off-the-shelf' commercial design, the Bell
407. Which is kind of ironic, because the Bell 407 is
a modern commercial version of the Bell 206 - the model the OH-58
was based on! And some of the UH-1 and OH-58A-C missions
will be taken over by the UH-72, which is the commercial
Eurocopter EC145. But the Army is still looking for a
replacement for the remainder of the UH-1 missions, and the
OH/MH-6 soldiers on with no replacement in sight, except maybe
the Fire Scout UAV, at least for some missions.
I don't think the issue is with the V-22 so much as with
Pentagon procurement policies in general. Almost every
major program in recent years has suffered cost overruns and
schedule delays. Even after suffering a major black eye on
aerial tanker acquisition, and knowing Congress and everyone else
was watching them closely, the USAF *still* royally screwed up on
the new tanker competition and had the GAO uphold Boeing's
protest and force a new competition. And this is also after
the GAO previously upheld protests over the SAR helicopter
competition, forcing a recompete there as well. You'd
think they'd learn from the repeated black eyes, but they
just can't seen to get it right these days. It seems to
be systemic.
As a teenager, I remember reading an editorial cartoon that seems
relevant. It showed a general and a ridiculous hodge-podge
weapons system. The first line, "At last we've got
a weapons system that is immune to attack." The last
line, "It's got parts built in all 435 Congressional
districts."
Sideline on air shows... In New York there's a place
called the "Rhinebeck Aerodrome". They still fly
aircraft from WWI and prior. Last time I was there they
flew a plane from 1910 (Berlioz?) with controls that worked by
wing-warping. They had a Fokker triplane (Red Baron) on
static display, and flew a Sopwith Camel. (Snoopy)
The airshow opens with a biplane in the air. The pilot
throws out a roll of toilet paper, then sees how many times he
can cut it with his wing as it unrolls toward the ground.
Report on Tiltrotor Osprey in Iraq
One of the more controversial aircraft ever deployed, the Osprey has suffered years of criticism. Here is a short report card with how the first batch of them are doing in Iraq. The gist of it is, still controversial going by the reports.
"The engine was breaking up. Not a good thing. But what's more interesting is the indication that the troubled engine was still putting out considerable thrust, but the aircraft couldn't maintain altitude," Bob Cox notes at Sky Talk. " The V-22 is supposed to be able to fly at least some distance and land on just one engine, but in this case it was unable to hold altitude while still getting significant power from the damaged engine. ed.z.: Has this plane ever been any good? I just don't recall much about it other than people thought it was an interesting idea, but the engineering left a lot to be desired.