Safir-1A (Rasad 1) |
Safir-1B (Navid-e-Elm-o-Sanat) |
Safir is an iranian space launcher based on the Kavoshgar-1 sounding rocket, which is a modification of the Shahab-3 IRBM.
The Safir-1 is a two stage vehicle with a stretched Shahab-3 (Nodong type) based first stage, a liquid fueled second stage with two engines. Safir-1A is a slightly improved version. The Safir-1B introduced an new fuel combination for higher thrust of stage one.
Possibly a small solid fuel third stage might be added to improve performance in future versions.
| Version | Stage 1 | Stage 2 |
|---|---|---|
| Safir-1 | Shahab-3 (str.) / ? | Stage 2 / 2 x ? |
| Safir-1A | Shahab-3 (str.) / ? | Stage 2 / 2 x ? |
| Safir-1B | Shahab-3 (impr. str.) / ? | Stage 2 / 2 x ? |
| Performance (kg) | LEO | LPEO | SSO | GTO | GEO | MolO | IP |
|---|---|---|---|---|---|---|---|
| Safir-1 | ~25 | - | - | - | - | - | |
| Safir-1A | ~25 | - | - | - | - | - | |
| Safir-1B | 60 | - | - | - | - | - |
No: Type Serial Date LS Payload
1 1 Safir-1 OES.0001 17.08.2008 F Sem Omid 2 2 Safir-1 OES.0002 02.02.2009 Sem Omid 3 1 Safir-1A UIS.0001 15.06.2011 Sem Rasad 1 4 1 Safir-1B ERS.2002 03.02.2012 Sem Navid-e-Elm-o-Sanat Planned: 5 2 Safir-1B . xx.xx.2012 Sem Fajr Launch Sites: Sem = Semnan Failures: Flight 1: Second stage lost control. Unclear, if orbital attempt or suborbital test flight.