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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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