Today in Kourou, French Guiana, Mr Fredrick Engstr¿m, ESA Director of Launchers, Mr Michel Courtois, Deputy Director-General of CNES and Mr Jean-Marie Luton, Chairman of Arianespace signed the document formally handing over Ariane launch complex ELA-3 from ESA to Arianespace.
Representing an investment of some 800 million ECU, ELA-3 is by far the
largest installation built by ESA under the Ariane-5 development
programme. CNES was responsible for its design, construction and
operation during cryogenic main stage testing and the first two qualification
flights, in its capacity as prime contractor for the development of the
Ariane-5 launcher and launch facilities. Arianespace will now take over
responsibility for ELA-3 operations, including launcher integration and
launch operations, final payload preparation, management and
maintenance of facilities, insurance, safety and quality control, in addition
to the similar responsibilities it has discharged since 1986 for the ELA-2
complex dedicated to Ariane-4.
Preparations for the hand-over of ELA-3 management responsibility to
Arianespace had been under way for some years, with the progressive
integration of Arianespace engineers and technicians into the CNES
teams, to ensure that personnel training was properly completed following
execution of the first two Ariane-5 qualification flights. Particular attention
has been paid to the industrial set-up in order to secure a coherent and
optimised structure meeting ELA-2 and ELA-3 operations & maintenance
requirements. To that end, Arianespace is contracting the same European
companies which have hitherto been working under CNES contracts.
Twelve firms (from Belgium, France, Germany, Italy and Spain) provide
some 250 specialists under operations & maintenance contracts for the
fluids and mechanical systems, computerised checkout systems, power
supply and air conditioning.
Arianespace also draws on the Guiana Space Centre's support services
for Ariane-5 launch campaigns, on the same basis as for Ariane-4
launches. These support activities, managed by CNES on behalf of ESA
with European contractors, include coordination of overall launch range
operations, ground and inflight safety, tracking and telemetry stations,
meteorology, telecommunications, operations & maintenance for payload
preparation facilities and logistical facilities.
Main features of ELA-3
The ELA-3 complex covers a 15 square km (3 x 5 km) area of land located
close to Ariane-4 launch complex ELA-2 and 25 km north-west of Kourou.
It is designed to handle a launch rate of eight to ten Ariane-5 launches per year at one month intervals. The duration of a standard launch campaign
will be 22 working days, once the necessary learning phase is over.
The basic ELA-3 design differs from that of earlier Ariane launch
complexes in that there is no mobile servicing gantry or umbilical mast in
the launch zone. This enhances the availability of the launch facilities and simplifies the launch zone itself, reducing its vulnerability in the event of an accident.
Construction work on ELA-3, which started in 1988, involved some two
million man-hours and sixty European companies providing the requisite
engineering design, construction and test expertise in the following areas:
infrastructures, power supply, air conditioning, mechanical structures,
specialised tooling, ground-to-launcher connections, cryogenic and
conventional fluids, computerized checkout systems, inspection, etc.
ELA-3 consists of two zones:
the launcher preparation zone, comprising:
the launch control centre, located in a 2700 square m protected
enclosure which is designed to withstand the impact of falling launcher
elements and includes:
two independent launcher checkout rooms, just one of which is fitted out currently,
one checkout room for ground utilities (power, air conditioning, fire detection, alarm systems),
three rooms for payload checkout;
the launcher integration building, 58 m high with an air-conditioned
interior of 80 000 cubic m where the solid-booster, main and upper
stages and vehicle equipment bay are assembled on a mobile launch
table. Assembly, electrical and tightness checks will be performed here
in a 13-day cycle, before roll-out to the final assembly building;
the final assembly building, 90 m high with an air-conditioned interior
of 123 000 cubic m where payloads are mated with their flight adapters,
encapsulated inside the fairing and hoisted onto the launcher. Assembly
of the launcher's upper section, the associated electrical checks and
upper-stage filling with propellants will be carried out here in a
8-day cycle before the launcher is finally rolled out to the launch
zone some hours prior to lift-off;
the launch zone, for final countdown and lift-off, comprising:
a solid base interfacing with the launch table, including the cryogenic
propellant (liquid oxygen/hydrogen) feedlines and launcher checkout
umbilical connections. It also has a wind dampening shield and four
lightning-conductor towers,
three separate flame trenches (one for the Vulcain engine and one for
each booster),
a 90 m high water tower with a storage capacity of 1500 cubic m for
table cooling and noise dampening on lift-off,
– connection facilities for the mobile cryogenic storage tanks,
a 310 square m gaseous hydrogen burn-off pool.
ELA-3 also comprises a 4 km twin railtrack for launcher roll-out and one
mobile launch table with an integrated umbilical mast (a second table is
due to be delivered in 1998). Each launch table weighs 870 tonnes
unladen, supports the launcher throughout its preparation campaign and
is fitted with a two-part 58 m high umbilical mast. The launch table/launcher
assembly, weighing 1500 tonnes, is towed by truck from the final assembly
building to the launch zone. In-transit power, ventilation and air-
conditioning requirements are met by a special servicing unit, while a
damper is used to absorb the energy generated by the action of the wind
on the launcher.
Between 1994 and 1996, the ELA-3 facilities were satisfactorily used for a
series of main stage firing tests, which ground-qualified the stage and the
ground facilities. The first two Ariane-5 qualification campaigns (501 and
502) proceeded without major technical problems regarding the ELA-3
ground facilities, which, with the improvements made to ange facilities
(safety, telemetry, downrange stations, etc.), are therefore considered as
qualified.
With the ELA-3 launch complex, other Ariane-5-dedicated production and
test facilities built during the development phase are being handed over
by ESA to the industrial operators at the Guiana Space Centre:
the Guiana propellant plant, for mixing and casting the large solid-
propellant booster segments, handed over in 1990 to Regulus, a joint
subsidiary of Fiat Avio (Italy) and SNPE (France);
the booster integration building, handed over in 1992 to
Europropulsion, a joint subsidiary of SEP (France) and Fiat Avio;
the booster preparation building, handed over in 1996 to Aerospatiale
(France);
the booster teststand, used for seven development and qualification
tests between 1993 and 1995 and to be used for quality-control test
firings on production units;
the liquid hydrogen plant, built and operated by l'Air Liquide (France).
