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The Atlas III (known as the Atlas II-AR (R for Russian) early in development ) was an American orbital launch vehicle, used in the years between 2000 and 2005. It was developed from the highly successful Atlas II rocket and shared many components.
- IIIA: 24 May 2000, IIIB: 21 February 2002
- 6, (IIIA: 2, IIIB: 4)
- 2
- Medium expendable launch vehicle
Language links are at the top of the page across from the title.
The Persian version of Wikipedia was started in December 2003. As of May 2024, it has 1,001,604 articles, 1,308,532 registered users, and 90,523 files, and it is the 19th largest edition of Wikipedia by article count, and ranks 22nd in terms of depth among Wikipedias.
- December 19, 2003; 19 years ago
- Persian
- 1,133,601 (total registered, as of 11 July 2022)
- Wikimedia Foundation (non-profit)
Aug 6, 2022 · Map of Iran in Persian. Topographic map. Provinces of Iran. Counties of Iran. History maps. This section holds a short summary of the history of the area of present-day Iran (Persia), illustrated with maps, including historical maps of former countries and empires that included present-day Iran (Persia). Fertile Crescent.
May 8, 2024 · Persia, historic region of southwestern Asia associated with the area that is now modern Iran. The term Persia was used for centuries and originated from a region of southern Iran formerly known as Persis, alternatively as Pārs or Parsa, modern Fārs.
- The Editors of Encyclopaedia Britannica
Introduction. This article deals with the government and politics of the great Persian empire which was founded by Cyrus the Great in the 540s and 530s BCE, and was conquered by Alexander the Great two centuries later. For this empire’s society, economy, religion, art and architecture see the article The Persian Empire: Culture and Society.
The single-stage Atlas IIIA booster uses a high-performance RD-180 propulsion system produced by a U.S./Russian joint venture (RD AMROSS) comprised of Pratt & Whitney (U.S.) and NPO Energomash (Russia). The RD-180 burns liquid oxygen and RP-1 propellant and develops a lift-off (sea-level) thrust of 2.6 MN.
