Ariane 4 - Variants

Variants

The rocket was used in a number of variants - it could be fitted with two or four additional solid (PAP - Propulseurs d'Appoint à Poudre) or liquid fueled booster rockets (PAL - Propulseurs d'Appoint à Liquide). The launcher included a satellite payload carrier system called Spelda (Structure Porteuse Externe de Lancement Double Ariane, French for 'External carrying structure for Ariane double launches') for launching more than one satellite at a time. The rocket captured nearly 60% of the world’s commercial launch services market, serving both European and international clients.

Ariane 4 AR 40 was the basic version, with three stages: 58.4 m high, a diameter of 3.8 m, a liftoff mass of 245 t and a maximum payload of 2100 kg to GTO or 5000 kg to Low Earth orbit (LEO). Main power was from four Viking 2B motors each producing 667 kN of thrust. The second stage had a single Viking 4B motor, and the third stage had an HM7-B liquid oxygen/liquid hydrogen motor. AR 44L, with the maximum additional boost of four liquid fuel rocket strap-ons, was four-stage, weighed 470 t and could transfer a payload of 4730 kg to GTO or 7600 kg to LEO.

Model PAL PAP Payload to GTO, kg Launches Successes Failure date
AR 40
-
-
2100
7
7
-
AR 42P
-
2
2930
15
14
1 December 1994
AR 42L
2
-
3480
13
13
-
AR 44L
4
-
4720
40
39
22 February 1990
AR 44LP
2
2
4220
26
25
24 January 1994
AR 44P
-
4
3460
15
15
-

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