Launch site for Iran's Safir space launch vehicle.
More... - Chronology...
Associated Spacecraft
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Omid Iranian technology satellite. 2 launches, 2008.08.16 (Omid) and 2009.02.02. First Iranian-built, Iranian-launched satellite. More...
See also
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Shahab Iranian derivatives of North Korean Nodong 1 intermediate range ballistic missile, evolved incrementally with Russian assistance into a longer-range missile and the first stage of an orbital launch vehicle. More...
Associated Launch Vehicles
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Safir-2 Iran's first orbital launch vehicle, based on the Shahab 3 intermediate range ballistic missile with upper stages. More...
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Seijil Iranian two-stage solid propellant intermediate range ballistic missile, with a range of 2,000 km. More...
Semnan Chronology
2000 September 21 - .
Launch Site:
Semnan.
Launch Vehicle:
Shahab 3.
LV Configuration: Shahab-3D.
- - .
Nation: Iran. Apogee: 1.00 km (0.60 mi).
2008 August 16 - .
19:32 GMT - .
Launch Site:
Semnan.
LV Family:
Shahab.
Launch Vehicle:
Safir-2.
FAILURE: Second stage failed catastrophically..
- Omid - .
Nation: Iran. Agency: IRSA. Class: Technology. Type: Technology satellite. Spacecraft: Omid. Apogee: 152 km (94 mi). Iranian suborbital launch in support of development of an indigenous satellite launch capability. Western analysts claimed it was a failed satellite launch attempt, and that the second stage of the launch vehicle failed catastrophically at 152 km altitude.
2008 November 12 - .
Launch Site:
Semnan.
LV Family:
Seijil.
Launch Vehicle:
Seijil.
- Iran RV - .
Nation: Iran. Summary: Technology payload..
2009 February 2 - .
Launch Site:
Semnan.
LV Family:
Shahab.
Launch Vehicle:
Safir-2.
LV Configuration: Safir-2 s/n 2.
- Omid - .
Mass: 25 kg (55 lb). Nation: Iran. Agency: IRSA. Class: Technology. Type: Technology satellite. Spacecraft: Omid. Decay Date: 2009-04-25 . USAF Sat Cat: 33506 . COSPAR: 2009-004A. Apogee: 373 km (231 mi). Perigee: 245 km (152 mi). Inclination: 55.5500 deg. Period: 90.70 min. Summary: First Iranian satellite launched by an Iranian launch vehicle..
2009 May 20 - .
Launch Site:
Semnan.
LV Family:
Seijil.
Launch Vehicle:
Seijil.
LV Configuration: Sejjil-2.
- Missile test - .
Nation: Iran. Apogee: 800 km (490 mi). Summary: Test.
2011 June 15 - .
09:15 GMT - .
Launch Site:
Semnan.
LV Family:
Shahab.
Launch Vehicle:
Safir-2.
- Rasad - .
Mass: 15 kg (33 lb). Nation: Iran. Class: Surveillance. Type: Surveillance satellite. Decay Date: 2011-07-06 . USAF Sat Cat: 37675 . COSPAR: 2011-025A. Apogee: 299 km (185 mi). Perigee: 236 km (146 mi). Inclination: 55.7000 deg. Summary: Satellite with an imaging payload..
2011 June 28 - .
Launch Site:
Semnan.
Launch Vehicle:
Shahab 3.
LV Configuration: Ghadr.
- Shahab RV - .
Nation: Iran. Summary: Operational test..
2011 June 28 - .
Launch Site:
Semnan.
LV Family:
Shahab.
Launch Vehicle:
Hwasong 6.
LV Configuration: Shahab 2.
- Shahab RV - .
Nation: Iran. Summary: Operational test..
2011 June 28 - .
Launch Site:
Semnan.
LV Family:
Shahab.
Launch Vehicle:
Hwasong 5.
LV Configuration: Shahab 1.
- Shahab RV - .
Nation: Iran. Summary: Operational test..
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