Discurso del Presidente Ahmadinejad en Ginebra

Payload (kg)100-500
700-1,000
Range (km)3,500-4,300 (2-stages)
4,000-4,300 (3-stages)
CEP (m)unknown
Diam. (m)2.2/1.3
Height (m)32
L. W. (kg)80-85,000
Thrust (Kg f)Effective: 30,432 per chamber
Actual: 31,260 per chamber
or
Effective: 104,204
Actual: 170,040
Burn time (sec.)<330?
Launch Acceleration (g's)~1.4-1.5 or 1.3
Thrust Chambers4, 1, 1
Stages2, 3
TypeLRICBM 
Stage 1Height (m)~16
Diameter (m)~2.2
Launch Weight (kg)~60,000-61,000
Launch Thrust (kg f)~102,880-104,000
Burn Time (sec.)~120-130
FuelTM-185
(20% Gasoline + 80% Kerosene)
OxidizerAK-27I
(27% N2O4 + 73% HNO3 + 
Iodium Inhibitor) 
Stage 2Height (m)~14
Diameter (m)~1.32-1.35
Launch Weight (kg)~15,200
Thrust (Kg f)Effective: ~13,160
Actual: 13,300-13,380
Burn Time (sec.)110 max
Isp. (sec.) Effective: 226 - SL
Due to vanes steering drag loss of 4-5 sec.
Actual: 230 - SL
Vac: 264 
Thrust Chambers1FuelTM-185
(20% Gasoline + 80% Kerosene)
OxidizerAK-27I
(27% N2O4 + 73% HNO3 + 
Iodium Inhibitor)
Propellant Mass (kg)12,912 
Stage 3Height (m)~3-4 total package
Diameter (m)~1.3-2.0 flared skirt type design
Launch Weight (kg)unknown
Launch Thrust (kg f)unknown
Burn Time (sec.)~100
PropellantSolid motor

Shafaq (Before the Dawn) 
The Shafaq / Shafagh / Shafag / Shakhab (Farsi for “before the dawn”) is a look-a-like of the YF-17. Shafaq is an advanced Light Attack/Trainer aircraft designed by the Aviation University Complex (AUC), part of the Malek Ashtar University of Technology. The Shafaq is reportedly a subsonic aircraft, made of radar-absorbing material. It has a large leading edge root extension (LERX) and a root aft of the wing which gives it an unusual circular sub-section. The Shafaq drawings show a subsonic attack aircraft with an empty weight of just over 11,000 pounds, an overall length of about 46 feet and a 39-foot wingspan. The design includes seven stores hardpoints–three beneath each wing and one beneath the aircraft’s fuselage centerline. 

Reportedly there are plans are to produce three versions -- a one-seat fighter, a two-seat light attack aircraft and a two-seat operational trainer. Other reports suggest that the Shafaq will be built in three variants, which include a Two-Seater Trainer, Two-Seater Light Attack and a One-Seater Light Attack variant. 

The design for a new Iranian light attack aircraft the appears to be a replay of a light fighter design developed around the end of the Cold War at the Mikoyan design bureau in Moscow. The original project of this plane was set forward for the Russian Air Force as both as a light multi-role fighter, and as an operational trainer. 

Developed at Malek Ashtar University of Technology in Tehran, the project was initiated as an "educational exchange program" with Russia. More than 20 designers formerly employed at leading Soviet design bureaus Mikoyan and Sukhoi went to Tehran to develop the aircraft’s planform and complete a full-up detailed design. 

Despite the obvious connection to previous Russian design studies, a Malek Ashtar University of Technology official named insisted that “this is not a Russian-inspired” idea and that the Shafaq "concept started in Iran and is finished in Iran." At the start of the program Iran received help from Russia, but Russia later backed away from this project and Iran carried on the project by itself. 

The otherwise unrenowned Soviet aircraft designer Fatidin Mukhamedov, D.Sc., said his company had been developing the "Integral" configuration since 1985. He said that multiple aerodynamic tests of various versions testified to the fact that the configuration can be used for aircraft of various types. Mukhamedov displayed the Shafaq design at the 1993 Dubai airshow, where the TOO 'Eurasia' company (later OKB 'Mukhamedov') introduced a long-term "integral" configuration combat aircraft project. Mukhamedov's first project was the "Eurasia-700" super capacity aircraft, unveiled in Le Bourget in 1993. 

In 2001, the "Integral" configuration was granted the first patent. This multi********nal fighter comprises a wing with a center wing embodied in the form of a profiled carrying disc provided with a leading and rear edge arranged along a generating line thereof. Outer wings are connected to the center wing. Each outer wing is embodied in a rotatable manner and equipped with a droop nose. It is claimed that the point of application of the summarized positive or negative ascensional power of the aircraft at the motion of the rotatable outer wings is maximum approaching the point of aerodynamic center point of the aircraft, making it possible to fly the fighter without changing a longitudinal moment thereof in the ascensional power controlling system. 

The Shafag program had been funded by the Islamic Revolutionary Guard Corps (IRGC) rather than the regular armed forces. 

As recently as late 2002 the first flight was supposed to happen in August 2004. By 2003 a 1/7 scale model of the Shafaq had completed testing in the AUC's wind tunnel and pictures had been revealed which showed that a Full-scale model has already been built. By 2005 all that was known to exist of the Shafaq, other than paper drawings, were models and a full-scale mockup that had been seen on Iranian television. By 2005 the aircraft was to be rolled out for flight tests in 2008.