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Sejjil
Iranian two-stage solid propellant intermediate range ballistic missile.
 Status: Retired 2008.  First Launch: 2008-11-11.  Last Launch: 2008-11-12.  Number:  2 . 
Subtopics
 | Ashura Iranian two-stage solid-propellant missile, evidently using some Shahab systems and its re-entry vehicle. | 
 | Sejjil-2 Iranian two-stage solid propellant intermediate range ballistic missile. | 
Country: 
Iran. 
2007 November 20 - . 
Launch Site: 
Semnan. 
LV Family: 
Sejjil. 
Launch Vehicle: 
Ashura. 
- Nation: Iran. 
Apogee: 300 km (180 mi). 
 
2008 November 11 - . 
Launch Site: 
Semnan. 
Launch Vehicle: 
Sejjil. 
- Sejjil-1 - . 
Nation: Iran. 
Apogee: 500 km (310 mi). 
 
- Iran RV - . 
Nation: Iran. 
Technology  payload.. 
 
2009 May 20 - . 
Launch Site: 
Semnan. 
LV Family: 
Sejjil. 
Launch Vehicle: 
Sejjil-2. 
- Missile test - . 
Nation: Iran. 
Apogee: 800 km (490 mi). Test. 
 
2009 September 28 - . 
Launch Site: 
Semnan. 
LV Family: 
Sejjil. 
Launch Vehicle: 
Sejjil-2. 
- Sejjil RV - . 
Mass: 800 kg (1,760 lb). Nation: Iran. 
Operational test. 
 
2009 December 16 - . 
Launch Site: 
Semnan. 
LV Family: 
Sejjil. 
Launch Vehicle: 
Sejjil-2. 
- Seijil test - . 
Nation: Iran. 
Test of two-stage solid-propellant IRBM, which Iran claimed was 'faster' (lower drag re-entry vehicel?) than earlier versions and had stealth capabilities. US authorities said they detected no different performance compared to earlier launches.. 
 
2010 Oct - . 
Launch Site: 
Semnan. 
LV Family: 
Sejjil. 
Launch Vehicle: 
Sejjil-2. 
- Sejjil-2 - . 
Nation: Iran. 
Agency: IR. 
Apogee: 800 km (490 mi). 
 
2011 Feb - . 
Launch Site: 
Semnan. 
LV Family: 
Sejjil. 
Launch Vehicle: 
Sejjil-2. 
- Sejjil-2 - . 
Nation: Iran. 
Agency: IR. 
Apogee: 800 km (490 mi). 
 
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