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Expendable LV's

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Angara
Ariane 4
Ariane 5
Athena
Atlas II
Atlas III
Atlas V
Avrora (Aurora)
Beal BA-2
Delta II
Delta III
Delta IV
Dnepr
Eurockot
GSLV
H-IIA
J-1
Kosmos 3M
Long March 3
Pegasus
Proton
Shtil
Soyuz
Start
Strela
Taurus
Titan II
Titan IV
Tsiklon
Zenit

   Atlas III - Summary
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wpe8.jpg (5042 bytes)The Atlas III vehicle is an improved version of the established Atlas II family of launch vehicles.  The prime modification was replacing the two Rocketdyne MA-5 first stage and single Rocketdyne MA-5 sustainer engines with a single NPO Energomash RD-180.  Furthermore, Lockheed Martin simplified vehicle construction by drastically reducing the total part count. 

Two versions of the Atlas III are currently available.  The Atlas IIIA has a single RL-10A-4-2 engine powering the Centaur upper stage while the Atlas IIIB has two RL-10A-4-2 engines and a stretched Centaur upper stage to increase GTO performance to just under 10,000 lb.  Both vehicles are being marketed by International Launch Services (ILS).

Prime Contractor: Lockheed Martin (Denver, CO)
Point of Contact International Launch Services, Inc.
1660 International Drive
Suite 800
McLean, Virginia 22102 USA

Tel:   571.633.7400
Fax:  571.633.7500
Launch Site: Eastern Test Range (28.7 deg. N Latitude)
Western Test Range (34.7 deg. N Latitude)
Web Links: Atlas III (ILS) Web Site
Atlas III Payload User's Guide
(4.8 Mb)

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