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Updated: Mon Jul 7 11:57:52 UTC 2008
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Ship
Integration - a Prerequisite
for New Navy Helicopters
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The US Navy (USN) Tarawa Class Amphibious Assault Ship USS TARAWA
(LHA-1) pulls alongside the Royal Australian Navy (RAN) Durance Class
(Underway Replenishment Tanker) (AORH) Her Majestys Australian Ship
(HMAS) SUCCESS (OR 304) to prepare for a replenishment at sea (RAS) in
support of exercise Rim of the Pacific (RIMPAC) 2004. A Westland Sea
King HAS 50/50A sits on the rear deck of the SUCCESS (Image US Navy).
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Air Power Australia Analysis
2007-03
16th May 2007
by Eli Manuel
Text © 2007 Eli Manuel
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Since the announcement of Government's
intention to replace Navy’s six remaining Westland Sea Kings in
2010[1]
with 46 NH Industries MRH90 helicopters, the ADF has designated the
NH90 the Multi Role Helicopter or MRH90, industry has also raised the
prospect of the MRH90 replacing the extant Sikorsky S-70B-2 Seahawk
in about 2016.
As far as this author is able to determine,
Australia’s 46 MRH90 helicopters are intended to be in the Army
configuration of the aircraft. This does not have the seagoing
modifications of the maritime variant. The purpose-built naval NH90
variant is called the NATO Frigate Helicopter or NFH90. The main
airframe differences between the NFH and NH90 includes the
incorporation in the former of a securing system, a powered automatic
main rotor blade folding system and floatation gear. In land based
operations these systems present a usually unjustifiable and most
significant weight and drag penalty. So the exclusion of navy
modifications is understandable for terrestrial operations. But their
absence “on the boat” presents a considerable
vulnerability and safety risk. It is surprising that the ADF with its
now considerable blue-water helicopter operating experience appears
to be again going down the path toward embarking on to ships
helicopters that are intended for land-based operations only.
None
of the other customers of the NH90, which is also designated in its
Army configuration as the Tactical Troop Helicopter or TTH, are known
to be planning to embark their NH90 in LPA-sized platforms such as
Manoora and Kanimbla or in aviation capable frigates like the RAN's
five Adelaide Class FFGs and eight ANZAC Class FFHs.
The French have reportedly conducted an embarked trial of the NH90
with their Mistral Class Landing Platform Dock (LPD). This large
platform is approximately three times the displacement of the RAN’s
LPA and with the Spanish Navantia is a contender in the ADF’s
Joint Project (JP2048) which intends to replace HMAS Tobruk and later
the 2 LPAs in about 2012 -2014. But the LPD is essentially an
aircraft carrier and as such is not considered a “small ship”
in the context of helicopter operation, as would be the LPA and the
RAN’s other air capable ships. The flight trial needed to clear
a combination of helicopter and ship throughout the intended flight
envelope has previously been a very lengthy process indeed and
involves many weeks of very scarce ships’ time. Traditionally,
Navy rather than the OEM or prime contractor, has borne the risk that
the eventual Ship Helicopter Operating Limit (SHOL) is less than that
specified as necessary.
A Royal Australian Navy (RAN) Visit, Board, Search, and Seizure (VBSS)
Team conducts a fast rope exercise from a hovering RAN S-70B-2 Seahawk
helicopter, onto the flight deck of the US Navy (USN) Dock Landing Ship
USS HARPERS FERRY (LSD 49). The Seahawk employs the RAST system (Image US
Navy).

US Army
UH-60A Blackhawk recovering on the USS Iwo Jima (LPH-2) in 1981 (US DoD
Image).

NFH-90
NATO Frigate Helicopter (Royal Netherlands Navy images).




NH-90
TTH
(Tactical Transport Helicopter) is the basis for the Army MRH-90
variant (NHIndustrie images)

An Australian Army UH-60 Black
Hawk helicopter from B Squadron, 5th
Aviation Regiment practices touch and goes aboard the U.S. Navy
Military Sealift Command Hospital Ship, the USNS MERCY (T-AH 19), off
the coast of East Timor in 2006 (US Navy image).
The operation of helicopters from
small ships is
very demanding and a high risk activity. Although the LPA’s now
routinely embark Army’s Black Hawk helicopters, these are
ordinarily operated in only calm conditions and sheltered waters.
Embarked Blackhawk operation is not usually considered a blue-water
capability. And the aircraft are not fitted with restraint, automatic
blade folding or floatation systems. However Navy’s Seahawks
and Sea Kings are fitted with automatic blade folding systems and
floatation equipment.
The Seahawk, which is routinely
embarked in the
FFG and FFH is also equipped to operate with the ship’s Curtis
Wright (previously Indal Technologies Inc) Recovery Assist, Secure
and Traverse (RAST) system. The RAST is attached to the landing
helicopter prior to, during and after touchdown. The system securely
holds the aircraft on the landing spot and enables it to be moved
safely in and out of the hangar in most sea states. The powered blade
folding system enables the rotor blades to be stowed without
personnel being required as was previously the case, to work on
safety critical flight controls some 4 to 5 meters above flight deck
level, sometimes in darkness, exposed to unpredictable ship movement
and continual wet from airborne salt sea spray. Some 200 RAST systems
are in service world wide. The major users include USA, Japan,
Taiwan, Canada and Australia.
Neither the NH90 nor NFH 90 is
known to be capable of operating with RAST.

An SH-60B Seahawk helicopter assigned to the Naval Air Warfare Center
Aircraft Division is hauled down to the Elevated Fixed Platform using
the Recover Assist, Secure Traverse (RAST) system during Dynamic
Interface testing (US Navy
image).

An SH-60B Sea Hawk helicopter takes off from the flight deck of the
guided missile frigate USS DOYLE (FFG-39). A carriage and tracks for
the ship's recovery assistance, securing and traversing (RAST) system
are on the deck below the helicopter (US Navy image).

An interior view of the recover assist securing traversing (RAST)
system control station aboard the guided missile frigate USS FORD (FFG
54) (US Navy image).
In terms of
operating capability and risk management, RAST is considered the
world’s most capable ship/helicopter restraint and handling
system for medium sized helicopters. But it requires heavy machinery
including embedded rails, winches, wires and control systems to be
“built into” the ship. It is not a system that can easily
be retro-fitted. The RAN has wisely made the decision to fit RAST in
all of its frigates. But the RAN’s other air capable ships are
without any such system and for securing aircraft therefore rely upon
personnel fitting chain lashings. Aircraft movement remains an
essentially “man-draulic” operation and depends upon a
large number of personnel carefully manoeuvring the aircraft around
the flight deck.
Relative to a RAST fitted ship,
flight deck
operations on a non-RAST ship present a high level of largely
unmitigated safety risk to the flight deck personnel and a high risk
of damage to the helicopter as a 10 tonne aircraft - the approximate
weight of a Seahawk, Sea King or NH90 - is difficult to safely
restrain and move on a pitching and rolling flight deck. Often the
heading and speed of the ship is constrained to those conditions that
provide the least deck movement - the deck motion limits for safe
manual aircraft movement are very small indeed - and relative wind.
But the required heading and speed is often not that required for the
ship’s mission. And no Commanding Officer likes to have his/her
freedom of manoeuvre restricted or to be exposed to increased risk of
air or subsurface attack for periods of about 30-45 minutes that
“spotting” (moving the aircraft from the hangar to the
landing/takeoff position) or stowing the aircraft in its hangar,
requires to complete. Many embarked aircraft have been damaged and
flight deck personnel injured by too hasty or violent ship
manoeuvring during helicopter operations.
In Australian waters
the most frequently occurring sea-state is 4 (ie Moderate with wave
heights of 1.25 to 2.5 metres) or above. As an approximation, Sea
state 4 can routinely produce LPA ship motion of greater than 10
degree roll. This is usually the limit for take and landing. But the
limit is much less for moving the aircraft manually around the
flight-deck and for folding and spreading main rotors or tail pylon.
Safe restraint of the helicopter beyond the take-off and landing roll
limit for a non-RAST ship is critically dependant upon manually
fitted chains. Flight deck personnel are again exposed to a high
safety risk moving around operating aircraft in usually wet and
dynamic conditions when of necessity, flight deck safety guard rails
are also lowered to provide additional physical clearance for the
helicopter’s flight.
The alternate restraint and
traversing system, and that which is usually fitted to the NFH90, is
based on an hydraulically operated probe and deck-mounted grid which
secures the aircraft before its takeoff and after landing. The
traversing operation is performed by a separate subsystem. And
several optional products are available. The Royal Navy uses the
probe, grid and a system of cables and winches to secure and move
embarked aircraft. DCN International of France markets a probe, grid
and a rail mounted traversing system. Manufacturers are understood to
include Claverham of the UK for the probe, RDM of the Netherlands for
the grid, MBB and McTaggart Scott for the traversing system. The
probe and grid system is fitted to approximately 350 ships worldwide
and it is usually a less costly but also a less capable system than
RAST. Aircraft fitted for operation to probe and grid systems cannot
operate to RAST or vice versa. Some helicopters such as the Westland
Lynx are optimised for operations to a flight deck and include
specialised undercarriage and negative main rotor thrust. Both of
these features tend to reduce an aircraft’s need for immediate
and positive securing.
Curtis Wright also markets an embarked
helicopter securing and traversing system called ASIST (Aircraft Ship
Integrated Secure and Traverse). The system provides a similar
operating capability as RAST but without the haul-down cable. ASIST
has been retrofitted to both FFG and MEKO (ANZAC) design frigates.
About 35 ASIST systems have been have purchased since 1995. Both The
Italian and German navies are understood to be fitting ASIST to their
NFH90 and their parent ships. But the certification status of ASIST
is not known. Maybe this is a less costly option than RAST.
Very
important ship and aircraft modification may be required if the ADF
is to embark the MRH90. Will the RAN modify its MRH90 for RAST? Or
will its RAST fitted ships be modified for probe and grid and a
wire-based traversing or some other system? Both questions could
drive procurement risk and therefore costs and schedule down the
familiar path followed by the RAN’s previous aviation projects.
Both possibilities have the potential to affect the RAN’s
ability to operate with the USN.
The clearance of a particular
aircraft in terms of the ability of its structure to sustain the
often severe loadings imposed by embarked operation usually depends
upon an evaluation of factors including the host ship’s
movement characteristics and the loadings imposed by the fitted
restraint and traversing systems. Even the position of flight deck
and hangar securing points can make a critical difference to aircraft
certification and its embarked fatigue life. The ADF has
traditionally taken a conservative approach to this matter. Therefore
the potential for delay in the certification of the MRH90 for
embarkation is seen as a hazard.
Manually folding a medium
sized helicopter on a moving flight-deck is an operation which for
most navies including the RAN, has presented an unacceptable safety
risk for about 20 years. Therefore the ADF’s Seahawk and Sea
King have powered folding systems. The breaking and remaking of
primary flying controls and surfaces required by the folding and
spreading evolutions requires absolute precision and the manipulation
of delicate and safety-critical components. Damage caused by manual
mishandling or dysfunction may not always be evident to a visual
inspection. The manual fold and spread method apparently conceived
for the MRH90 is assessed as likely to impose severe operating
constraints and a high risk of damage and injury. It is not clear how
that risk can be effectively mitigated other than by not undertaking
the evolution.
The operation of the MRH90 without floatation
equipment will mean, as it presently does for the Blackhawk, that the
aircraft will sink when it, for whatever reason, enters the water.
The aircraft’s inability to float obviously presents a very
considerable safety risk to incapacitated aircrew or passengers
because they may be unable to escape. The cause of the ditching may
also be lost to further investigation. It is unclear how these risks
are intended to be mitigated. Modular floatation gear may be
available for the MRH 90. But the ability of this to sustain the
aircraft on the surface, in an upright attitude and in typical sea
states is not known.
All of these factors may be under
effective consideration by the MRH90 procurement project. But no
discussion about the ship integration features needed to embark MRH90
has been seen.
In conclusion, the essential
questions are
summarised as follows:
-
What is the MRH 90’s embarked
concept of operation?
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What classes of ship is the MRH 90
formally cleared to operate to and be embarked in?
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Are powered blade
folding/spreading, floatation equipment and a securing and traversing
system intended to be fitted to the MRH 90 for its embarked service?
What operating envelopes are required to be provided by these systems?
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What is the duration of First of
Class Flight Trials scheduled for each of the ship classes intended to
operate the MRH 90? And, what operating envelope in terms of ship
motion and relative wind is sought in each case?
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Is it intended that the MRH 90 be
modified to operate with the RAST systems fitted to our FFG’s, Anzacs
and USN air capable ships?
-
What is the commonality between
NFH and MRH 90?
-
What formal responsibility does
the prime contractor have for the embarked Ship Helicopter Operating
Limit (SHOL) and airframe certification achieved by the MRH 90?
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| [1] Janes Defence Weekly of 28th June 2006 |
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| Air Power Australia
Analyses ISSN 1832-2433 |
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Artwork, graphic design and text © 2004, 2005, 2006, 2007 Carlo Kopp; Text © 2004, 2005, 2006, 2007 Peter Goon; All
rights reserved. |
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