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Updated: Sun Aug 29 16:43:38 UTC 2010
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APA NOTAMS ISSN 1836-7135
JSF F-35 Program: How Many Miles
Does an F-35A Go On a Tankful of Gas?
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Air Power
Australia - Australia's Independent Defence Think Tank
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Air Power Australia NOTAM
6th April, 2009
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| Contacts: |
Peter
Goon
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Carlo
Kopp |
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Mob:
0419-806-476 |
Mob:
0437-478-224 |
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Aerial
refuelling of F-35A AA-1 from KC-135R tanker (US DoD image)
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If you live in the boondocks where it is a long
way between gas stations, then when you purchase a new SUV, one of the
Key
Performance Parameters (KPPs) you ask the
salesman
is how far a tank of gas will take you. Being
out of fuel in the middle of
Death Valley with the midday sun blazing down is no
picnic.
And
so it is with aircraft, especially air combat
aircraft that must fly to a target area, engage the enemy, then
fly home. If you have the range to deliver
a war-load a long way, then you
keep
the bad guys away from your AWACs and
tankers, or
better still, fly the whole mission without vulnerable Low Density /
High
Demand (LD/HD) support.
In
August 2002, Colonel
Dwyer
Dennis of the Joint Strike
Fighter Project Office was briefing his
buddies
‘down-under’. This was in the
halcyon days when the JSF project was on-track, on-time
and on-cost. The role of KPPs was discussed, and the Colonel noted:
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“I'm going to
talk a little bit about what we call KPPs,
or Key Performance
Parameters. The key performance parameters on a program are those
requirements that are the make or break on a program.
You
miss a KPP and your
program is subject to cancellation or major rework.
…….”
“One
thing that I didn't talk about earlier, ….,
is that because this is a stealth aircraft it has internal weapon bays
and to
make it stealth the weapons have to be internal in a low-observable
mode, so
that makes the plane pretty thick and so that gives you a lot of room
for fuel.
So these aircraft have tremendous range.”
“The
CV
variant is outward to almost 700 -…
the Air Force I think about 590.”
“So
very
significant range. That's no external fuel tanks, just the internal
mission
fuel. …
To give you an idea of the
internal fuels - 18,000-plus for the CTOL, 13,000 for the STOVL and
over 19,000
pounds for the CV aircraft.”
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The JSF has over 430 KPPs designated, all of
which are
‘project
critical’, with the radius of
action being one of these. If the JSF fails to meet or
exceed that KPP, then, according
to the Colonel, the
consequences for the JSF project would be extremely
serious, as in ‘project cancellation’ or ‘major rework’.
And
so it should be! To
do otherwise is, at best, just
silly.
Why
do intelligent buyers specify KPPs?
Well,
the operations research defines what
capabilities are required, and the KPPs
are then set
as the criteria which decide on a ‘buy or
no-buy’
decision. Should an aircraft
manufacturer achieve the designated KPPs? You bet, otherwise any piece of rubbish
will do, and there will
be failures, some
spectacular, when you take an air combat aircraft into a shooting war.
When
should KPPs be
tested?
An
intelligent buyer will demand that achievement
of a KPP should be demonstrated at the earliest possible time. If the aircraft fails to meet the
designated KPP, then there is the greatest possible time to redesign
the
aircraft, or if it cannot be successfully redesigned, scrap the project
and
seek alternative way of meeting the capability requirements.
Who
should be accountable
for testing JSF KPPs?
Commonsense
suggests that it
should
be the Joint Strike Fighter Project Office since they define their
‘mission
statement’ as:
“The
Joint Strike Fighter (JSF) Program, formerly the Joint Advanced Strike
Technology (JAST) Program, is the Department of Defense's
focal point for defining affordable next generation strike aircraft
weapon
systems for the Navy, Air Force, Marines, and our allies.” (Refer http://www.jsf.mil/program/).
This
is a curious
and
worrying statement, also from the
mission statement:
“The
focus of the program is affordability -- reducing the development cost,
production cost, and cost of ownership of the JSF family of aircraft.”
The focus is
‘affordability’? Should
not the focus be ‘effectiveness
in future air combat’?
There
is also this key
question: is the JSFPO buying or selling the F-35 Lightning II?
While
many naturally assume that the ‘Purchasing
(i.e. Program) Office’ is charged
with conducting Caveat Emptor activities
on
behalf of the US Department of Defence and the US’s Allies, many of the recent
statements of
the JSFPO’s Program Executive Officer
sound distinctly
like
the
JSFPO
is selling
the
aircraft rather than buying it. And if the JSFPO and the PEO
are not
conducting Caveat Emptor
activities
like testing achievement of KPPs, then who
is?
Notwithstanding,
we seem to be at
the point where the JSF can
demonstrate a ‘mission
critical’ KPP like the un-refuelled combat
radius
of action. This KPP has been
set at
a minimum of 590 nautical miles, or 1180 nautical
miles in a straight line. The
combat load should be defined by the KPP – perhaps 2 x 2,000 lb JDAM, 2
x
AIM-120 or 2 x
AIM-9X. The fuel reserves should also be
defined – perhaps 30 minutes of useable fuel, that
being in
excess of the fuel required to cool the JSF’s
systems.
The
JSF recently demonstrated its ability to fly a
sortie of this distance – the
repositioning of aircraft AA-1 from Ft Worth NAS in Texas to Edwards
Air Force
Base in California – a great-circle distance of 1041 nautical miles. Unfortunately, testing
the
un-refuelled combat radius KPP was not possible on this flight because
the JSF
was accompanied by a Tanker, and AA-1 had a
couple of
drinks along the way.
The
Development Test and
Evaluation mission profile for the
un-refuelled range KPP is easy to set-up. Fill the internal fuel tanks of a CTOL
JSF to the maximum capacity; load the
aircraft with a representative weapon configuration; then, with a
representative
pilot at the controls, fly the designated USAF sortie profile.
Total
planned flight
distance
should be at least 1180
nautical miles. Lockheed Martin might like
to use a ‘fly-out fly-back’ track, so that
the
test pilot can monitor fuel burn and adjust the distance flown – either
increasing or decreasing distance flown to arrive
overhead the destination airfield with 30 minutes holding. On shut-down, the JSF would be refuelled to ‘full
tanks’ so
that the fuel burn along the way would be exactly established. A few sums, and the un-refuelled range
could be
shown to be either a ‘pass’ or a ‘fail’ against
the
590 nautical mile KPP.
Of
course, the whole exercise should be monitored
by independent agencies, perhaps
key
customers such as the USAF and US’s
Allies interested in purchasing the JSF, and the
measurement process assisted by the Defence
Science Board and the Government Accountability Office. These Agencies would
confirm
that the test JSF was fully
fuelled, that the
claimed
distance flown was accurate,
the stated fuel burn was exact and
the
allowance for wind along the way a true measure, and,
importantly, that the
required fuel reserves were preserved, including
fuel required for systems cooling. They
would then independently calculate the un-refuelled
combat range.
The
JSF should be accompanied by an escort
aircraft to ensure both aircraft stay on
track; to
independently measure the distance over the ground; measure
wind
aloft along the flight path; and, to render
assistance in the event of an emergency.
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| Likelihood |
Consequence |
Insignificant
1 |
Minor
2 |
Moderate
3 |
Major
4 |
Catastrophic
5 |
| Almost certain |
H |
H |
E |
E |
E |
| Likely |
M |
H |
H |
E |
E |
| Moderate |
L |
M |
H |
E |
E |
| Unlikely |
L |
L |
M |
H |
E |
| Rare |
L |
L |
M |
H |
H |
| Legend: |
| E– |
Extreme
level of risk (Immediate
action required by Executive and Directing Governance levels, i.e. do
not proceed with activity until this level of risk is reduced) |
| H– |
High
level of risk (Executive Management
attention required) |
| M– |
Moderate
level of risk (Able to
delegate to Implementation Management Level with ongoing Executive
Management oversight) |
| L– |
Low
level of risk (Able to be
managed through routine procedures) |
Table
1: Risk assessment
process and associated template of AS/NZS 4360:2004 (P.A. Goon).
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To add interest, the JSF
might be accompanied by an
F-15E Strike Eagle carrying the same test weapons
load: 2 x 2,000 lb JDAM, 2 x AIM-120 or 2 x
AIM-9X. My flight manual for the
Strike Eagle is out-of-date as it only has performance figures for the old F100-PW-200
engines. Even so, with 30 minutes
of holding at the destination, retaining all stores and with Lantirn Navigation and Targeting
pods fitted, the
combat radius is 945 nautical miles or 1,890 nautical miles in a
straight line. Escorting the JSF will
force the F-15E
to fly a slower, lower, sub-optimal flight profile, but as this
aircraft has
‘fuel to burn’, it should have no trouble providing
escort to the JSF on this important test run.
Combat
radius of action is rightly a critical Key
Performance Parameter. Failure to meet
or exceed this KPP is also
rightly
a critical element of a go no-go decision for the JSF program, refer
Table 1.
The
flight of JSF AA-1 from Ft Worth to
Edwards Air Force Base was a proving flight that
demonstrated there are no
impediments to the critical un-refuelled range KPP being able
to
be demonstrated in the
very
near future.
So,
please Mr
Lockheed
Martin, how many miles do we get from
a tankful of gas in a JSF?
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Air
Power Australia Website - http://www.ausairpower.net/
Air Power Australia Research and
Analysis - http://www.ausairpower.net/research.html
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