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	Ariane (rocket) - Wikipedia, the free encyclopedia
		Ariane is a series of a civilian European expendable launch vehicles for space launch use.
		Ariane 5-ECB, with further improvements intended to carry 12 tonnes into geostationary transfer orbit, was cancelled in May 2005 due to lack of demand.
		A 4.5 metre long and 85 kilogram heavy flyable model of the Ariane 4, which was built by a working group of the ARGOS, was launched 2002 in Amarillo, Texas and on 19 September 2004 at 12.15 o'clock successfully in the Val de Ruz near Neuchatel, Switzerland.
	en.wikipedia.org /wiki/Ariane (677 words)

	Ariane
		Ariane 1 flew 11 times from 1979 to 1986, failed twice, and launched a number of communications and other satellites, and the Giotto probe to Halley’s Comet.
		The first and third stages of the Ariane 2 and 3 were lengthened from those of their predecessor to enable a longer burn time, and the engines of stages one, two, and three were increased in thrust.
		Ariane 5’s 17,500-kg LEO (low Earth orbit) payload capacity was intended to accommodate the Hermes space plane.
	www.daviddarling.info /encyclopedia/A/Ariane.html (616 words)

	Ariane 1, 2, and 3 from the ESA
		Ariane 1 was designed primarily to put two telecommunications satellites at a time into orbit, thus reducing costs.
		Ariane 3 made a record 11 flights from 1984 to 1989, all of which were successful.
		The first and third stages of Ariane 2 and Ariane 3 were longer than those of Ariane 1, while Ariane 3 had strap-on boosters containing liquid or solid propellant, making it the most flexible and powerful of the three launchers, able to launch a payload of 1.7 tonnes.
	www.spacehike.com /esaariane123.html (287 words)

	Cnes - ARIANE 1 to 4
		Within 12 years Ariane 1 to 4 had launched over half of the commercial satellites in the world.
		The more powerful Ariane 5 has now taken over, with the objective of confirming European dominance in the civil launch market, in spite of stiff competition from the US, Russia, China and Japan.
		Ariane 5 - Europe’s launcher for the 3
	www.cnes.fr /html/_455_461_1375_.php (234 words)

	FLUG REVUE November 1997: 100th Ariane launch succeeds
		Ariane 1 could carry a 1750-kilogram payload into a geostationary orbit.
		Ariane 5 was projected to consist of the first stage of Ariane 4 in combination with a cryogen second stage.
		With Ariane 5, that was the understanding in 1979, it would be possible to carry space stations or the European space shuttle Hermes.
	www.flug-revue.rotor.com /FRHeft/FRH9711/FR9711c.htm (771 words)

	Kourou
		Ariane 2/3, Ariane 4, Ariane 42L, Ariane 42P, Ariane 44L, Ariane 44LP, Ariane 44P.
		Launch time 1119:33 UT. Positioned in geosynchronous orbit at 1 deg E in 1988-1989; 49 deg W in 1989; 4 deg W in 1990-1991; 49 deg W in 1991-1993; 75 deg W in 1993-1995; 70 deg W in 1995 Last known longitude (5 September 2001) 175.17 deg W drifting at 11.970 deg W per day.
		The Turksat 2A (Eurasiasat 1) satellite was an Alcatel Spacebus 3000B3 with a dry mass of 1577 kg (launch mass 3535 kg) and a 37m solar panel span.
	www.astronautix.com /sites/kourou.htm (11902 words)

	Ariane 1 (Site not responding. Last check: 2007-10-08)
		Ariane I is the first version of the Ariane launcher family.
		With lift-off mass of 210,000 kg, Ariane I was able to put in geostationary orbit one satellite or two smaller of a maximal weight of 1850 kg.
		The Giotto mission's spaceprobe was successfully launched on the tenth Ariane 1 (flight V14) on July 2, 1985.
	www.worldhistory.com /wiki/A/Ariane-1.htm (272 words)

	Spaceflight :Arianespace and the Ariane Family of Rockets
		Ariane 1, March 4, 1984, payload was Intelsat V F8.
		Ariane was the centerpiece of the European Space Agency (ESA) during its early years.
		Industry analysts note that although Ariane may not be the cheapest launch vehicle available, even in the dual launch configuration, Arianespace's customer service and flexibility—such as a launch range free of other military or human spaceflight launches—makes it a highly-effective competitor.
	www.centennialofflight.gov /essay/SPACEFLIGHT/ariane/SP42.htm (1561 words)

	Ariane 1 - 4
		Ariane was optimized for launches in GTO to which it could deliver 1750 kg.
		The flexibility of Ariane 4 is due to the adaptation of the payload by addition of boosters on the first stage.
		Its mass ranges from 243 tons (Ariane 40) to 480 tons (Ariane 44L) and the GTO performance from 2020 kg to 4460 kg.
	www.sat-net.com /serra/aria14_e.htm (824 words)

	[No title]
		Centaure 1 - 2 Belier - - 1 150 -6300 ?
		LM AS - 1 LM AS - - 1 0 0 LS-A - 1 LS-A Booster - - 1 5 -6378 ?
		NATIV - 1 RTV-A-3 - - 1 15 -6378 NOTS 401A Sandhawk - 1 NOTS 401A - - 1 20 -6378 NOTS 401A Sandhawk - 2 Sandhawk - - 1 250 -6300 ?
	www.planet4589.org /space/lvdb/sdb/LV_Stages (12667 words)

	Ariane 1
		Positioned in geosynchronous orbit at 26 deg W in 1982-1986; 178 deg E in 1986-1991; 20 deg E in 1991-1992; 22 deg E in 1992-1996 Last known longitude (1 September 2001) 11.08 deg W drifting at 18.839 deg W per day.
		Geostationary position 10+/- 0.1 deg E. EUTELSAT 1 is a regional geostationary telecommunication Satellite for European countries.
		Positions: Document Positioned in geosynchronous orbit at 10 deg E in 1983; 13 deg E in 1983-1989; 16 deg E in 1989-1991; 25 deg E in 1992-1993; 48E1993-1996; 36 deg E in 1996 Last known longitude (31 August 2001) 12.27 deg W drifting at 5.043 deg W per day.
	www.astronautix.com /lvs/ariane1.htm (1515 words)

	What is a launcher - Past - Ariane 1/2/3 (Site not responding. Last check: 2007-10-08)
		Ariane, which first flew in December 1979, was designed primarily for putting telecommunications satellites into orbit two at a time to reduce launch costs.
		As the size of satellites grew, Ariane 1 gave way in 1984 to the more powerful Ariane 2 and Ariane 3, and these in turn were superseded by Ariane 4 in 1988.
		Ariane 2, 3 and 4 all belonged to the same family but with certain differences.
	industry.esa.int /ATTACHEMENTS/A8604 (205 words)

	ARIANE 1 to 3 - Developmental launchers
		For the first time in the history of the space adventure, a heavy 3-stage launcher capable of placing a nearly 1-tonne satellite in geostationary orbit was successfully sent aloft.
		The most important modification for Ariane 3 was the addition of 2 solid-fuel boosters to the first stage of the rocket.
		Ariane 3's first flight successfully took place on 4 August 1984 with the launch of the ECS 2 and Telecom 1A satellites.
	www.cnes.fr /html/print-_455_461_1375_1377_.php (322 words)

	ESA - Launch vehicles - Ariane 5 Generic
		Since it became operational Ariane 5 has been used to launch satellites for communications, Earth observation and scientific research.
		In order to launch Ariane 5, ESA built a new launch site at Europe’s Spaceport in Kourou, as well as facilities to integrate the solid boosters and a plant to produce the solid propellant they use.
		Ariane 5 is used for launches into geostationary transfer orbit, medium and low Earth orbits and Sun-synchronous orbits.
	www.esa.int /SPECIALS/Launchers_Access_to_Space/SEM9UD67ESD_0.html (117 words)

	Ariane-1 (Site not responding. Last check: 2007-10-08)
		Serial Type TypeNo Date Orb Payload -------------------------------------------------------------------------------------------------------------------------------- 1 L-01 Ariane-1 1 24.12.79 CAT 1 2 L-02 Ariane-1 2 23.
		6.83 G ECS 1 / Amsat P3B (Oscar 10) 7 L-7 Ariane-1 7 19.10.83 G Intelsat-5 7 8 L-8 Ariane-1 8 5.
		5.84 G Spacenet 1 14 V-14 Ariane-1 10 2.
	www.skyrocket.de /space/doc_lau_det/ariane-1.htm (147 words)

	From Ariane-1 to Ariane-5
		This is mainly due to Europe's political will to back the programme in order to achieve the best possible end result (launcher, launch base and services), developed and produced in a suitable structure fully geared to market requirements and capable of standing upto the competition.
		Ariane's successes came thick and fast in the early eighties and today Ariane is the yardstick for success on the world launch services market, thanks to:
		The table below shows the launchers (with their GTO lift capability) which are or will be competing with Ariane in the near future.
	esapub.esrin.esa.it /rfs/rfs16/guer16.htm (1141 words)

	CSG Kourou (Site not responding. Last check: 2007-10-08)
		The Ariane launch complex (ELA-1) used the infrastructure developed for the Europa II launchers, with some adaptations of which a lengthening of the assembling tower.
		The ELA-1 was used 25 times for Ariane 1 to 3 launches until 1989, then it was dismantled in 1991.
		This unit was used for the first time in March 1986 and should remain in service until the Ariane 4 withdrawal, after year 2000.
	www.univ-perp.fr /fuseurop/kourou_e.htm (599 words)

	Space Launchers - Ariane
		When Ariane 4 is launched in this configuration, the propellant tanks of the first and second stages are not completely filled.
		Ariane 3 used the Sylda for dual launches, encapsulating the lower satellite and mounting the forward payload on its front face.
		The 880 kg Speltra, the equivalent of Ariane 4's Spelda, increases the length of the upper composite by 5.66 m and permits the launch of double payloads.
	www.braeunig.us /space/specs/ariane.htm (1710 words)

	Ariane 1 resources (Site not responding. Last check: 2007-10-08)
		First launched in Dec 1979, the Ariane 1 became the forerunner of the first commercially successful launch vehicle.
		The Ariane 1 Model The Ariane family lineup
		Ninfinger's Quick Look review of the kit (Sven "Ninfinger" Knudson is an independent reviewer).
	sputnik.freehomepage.com /Models/Ar1.html (53 words)

	Ariane 1
		Ariane 1 L01 - Ariane 1 L01 - COSPAR 1979-104
		Mode B (435 MHz uplink and 145 MHz downlink) transponder and 145 MHz beacon.
		Marecs B intended for maritime communications, planned for lease to Inmarsat; launched with Sirio 2.
	www.friends-partners.org /partners/mwade/lvs/ariane1.htm (1106 words)

	[No title]
		2A - CSG ELA2 - Arianespace OS Sat CNES32 - 1992-010 2448679.50 1992 Feb 26 2358:10 Ariane 44L 44L V49 Superbird B1/Arab 1C - CSG ELA2 - Arianespace OS Sat CNES32 - 1992-021 2448728.48 1992 Apr 15 2325:27 Ariane 44L 44L+ V50 Inmarsat 2F4/Tel.
		1/Meteosat 6 - CSG ELA2 - Arianespace OS Sat CNES32 - 1993-078 2449339.56 1993 Dec 18 0127:00 Ariane 44L 44L+ V62 DBS 1/Thaicom 1 - CSG ELA2 - Arianespace OS Sat CNES32 - 1994-F01 2449377.40 1994 Jan 24 2137:00 Ariane 44LP 44LP+ V63 Eut.
		B1 - CSG ELA2 - Arianespace OS Sat CNES32 - 1994-058 2449604.52 1994 Sep 9 0029:44 Ariane 42L 42L+ V67 Telstar 402 - CSG ELA2 - Arianespace OS Sat CNES32 - 1994-065 2449633.55 1994 Oct 8 0107:00 Ariane 44L 44L+ V68 Thaicom 2/Solid.
	www.planet4589.org /space/lvdb/launch/Ariane (195 words)

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