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Iran's first space launch vehicle Safir
IRILV
Norbert Brügge, Germany
Update: 05.02.2010
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TEHRAN, 2008,
Feb. 4 -- Iran launched probably their first space launch vehicle
"Safir IRILV" and revealed the Iranian launch site nearby Semnan
to be used for launching satellites into LEO. The launch site involves an underground
control station and launch pad to be used to fire an Iranian satellite named
"Omid" into space. The satellite "Omid" built by Iranian scholars is
the first domestically-made satellite to be set at a low earth orbit.
The Iranian press presents first photos of the new SLV and their propulsion.
The named Safir IRILV (Islamic Republic of Iran Launch Vehicle) is standing
on the Space Industries Group Center in Tehran.
The current launch was not shown. It was shown however the launch site with
a launch-tower in the desert. In the meantime there are pictures of the rocket
from the transport to the launch site.
The confusion is great in the world-press because the messages and pictures
from the Iran are contradictory to the launch. The presented videos are probably
old. They show the launch of the sounding rocket Kavoshgar from February 2007.
The Kavoshgar is based on Shahab-3M missile.
The shown launch pad is the launch pad for the Safir IRILV, which was under
construction in 2007 at the same location.
A sequence at the end of a Iranian launch-video a striking structure shows
in the sky. It looks like a disaster. This sequence does not belong to the
launch from the Kavoshgar sounding rocket. Probable is that an extra sequence
from the current failure of the Safir IRILV. It had with high probability the
satellite Omid on board. The probability is high, that Iran on the occasion
of the anniversary of the revolution had the ambition, to transport a satellite
in an orbit. That has failed evidently.
The surprise is great. The two-stage rocket Safir IRILV is composed of a first
stage Ghadr-II (similar Nodong++)
and a shorter second stage of equal diameter of 1.25 m. The vehicle has a length
of approximately 22.4 m.
A Scud missile is not used as second stage. It is however a liquid propellant
stage, which is propelled by two small engines. They are two single engines
with nozzle extension.
The engines are similar to a small
Soviet engine. The partially application of the Soviet
R-27 SLBM technology
is recognizable. The turbopump and their arrangement is similar to the Soviet
R-27 turbopump.TEHRAN, 2008,
Aug. 16 -- Iran says, it successfully launched its two-stage rocket Safir
IRILV to transport a dummy of the Omid satellite in orbit. The test-satellite
is named Safir-e-Omid.
Probable this was the next however not successful attempt to transport the
satellite "Omid" in the orbit. Up to now no data of the orbit were made known.
However there were shown new details of the rocket and from the lift-off itself.
TEHRAN, 2009, Feb. 3 -- Iran
has sent its first home-built satellite into orbit, Iran's English-language
satellite news channel Press TV reported. The Omid lightweight telecommunications
satellite was sent into space by the Iranian-produced satellite carrier Safir
IRILV, the report said. Equipped with two frequency bands and eight antennae,
Omid will transmit information to and from earth while orbiting the planet
15 times an hour, Press TV said. The satellite is also equipped with remote
sensing, satellite telemetry and geographic information system technology,
as well as remote and ground station data processing.
The first Iranian satellite was launched into orbit on a southeastern trajectory.
Two objects are in orbits of 245 - 378 km; 55.51 deg and 245 - 439 km; 55.6
deg. One is presumably the Omid payload and the other the Safir rocket final
stage, but it's not clear yet which is which. The Iranian News Agency calls
the launch vehicle Safir-2. Pictures of the launch show "Safir - Omid (2) IRILV"
painted on the side of the rocket. However is it probably the third launch.
The first vehicle was launched under another logo.
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The launch 2008, Feb. 4 |
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First Safir IRILV on the Space Industries
Group center in Tehran
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A sequence at the end of a Iranian launch-video a striking structure shows
in the sky. It looks like a disaster. This sequence does not belong to the
launch from the Kavoshgar sounding rocket.
Probable is that an extra sequence from the current failure of the Safir IRILV.
It had with high probability the satellite Omid on board. The probability
is high, that Iran on the occasion of the anniversary of the revolution had
the ambition, to transport a satellite in an orbit. That has failed evidently. |
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The first failed Safir launcher (2008,
Feb. 4)
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Is that the failure of the first Safir
launch ? >>>>>>>>>>
Video
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The launch 2008, Aug. 16 |
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Launch
video *
Launch video
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Launch pad before the completion
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Semnan space launch site: 35°14' 04"N
/ 53° 55' 20"E
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Pre-launch
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Safir IRILV at the launch-tower
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The launch 2009, Feb. 3 |
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Vehicle on launch pad
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Launch vehicle
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Upper stage with fairing
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Safir first stage rear
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Safir rocket is ready
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Lower part of the first stage tank
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First stage upper part
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Nose-cone
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| Propulsion |
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Combustion chamber injector plate
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Comparison between Nodong and Scud engine

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In FARSI: FIRST STAGE SAFIR ENGINE
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Enclosure of the second stage turbopump

Second stage engine with nozzle extension

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The turbopump


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in FARSI: The SECOND STAGE SAFIR
ENGINE
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Rear of second stage: Engines
with their nozzle extension
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Possible technical data
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Stage
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Engine
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Thrust s.l.
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Isp s.l.
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Thrust vac
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Isp vac
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Propellant |
Burn time
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Flow rate
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Total Imp
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-
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-
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kN
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N*s/kg
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kN
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N*s/kg
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tons
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s
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t/s
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MN*s
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1
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Nodong
(1)* |
283,8 |
2417 |
313,8 |
2672 |
UDMH/AK-27S |
15,259 |
130 |
0,1174 |
40,8 |
| 2 |
n.n (2) |
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73,5 |
2844 |
UDMH/AK-27S |
3,876 |
150 |
0,0258 |
11,0 |
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*
Isayev n.n. (= YF-3/Scud-D/Nodong engine)
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Iran's next satellite Ya Mahdi ?
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Key organizations
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