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Iranian Space program

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If it ever exists... no design (except yours ) , no info , no unveil ( without a single launch one does not simply talk about its payload ) and if the so called sepehr is just a safir 1 with some boosters then let me tell you it can't put anything more than 200 kg into orbit.... It seems that qoqnoos is cancelled too . And i am happy if they cancel all these safir simorgh sepehr and put their energy, time and money on something practical ( maybe qaem ) with 500+ kg payload and 500+ km stable orbit .

You designed it as sepehr . right ?
Simorgh_2B[1].jpg
 
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TEHRAN, 2012, March 05 -- Information by Mehdi Farahi, Director of the Aerospace Industry Organization:
Safir-2A is the first version of Safir-2 with the name of Simorgh. Length of it is 26 m, diameter of it is around 2.5 m and weight of it is around 86 tons. Thrust of is around 143 tons. It can put 100 kg satellites into 500 km altitude orbits.
The next our step is Safir-3A (Sepehr) and Safir-3B (Sarir) that can put 1,000 kg satellites into 1,000 km altitude orbits. If could add micro thrusters and some side equipments to it, it can put payloads into 36,000 km altitude orbits.
The design and production of satellite carrier rockets with a range of 1,000 kilometers are given a high priority in the country’s Five-Year Development Plan (2010-2015).
Iran aims to send other satellites into geostationary orbits, around 36,000 kilometers above the Earth's equator, after the end of the country’s Five-Year Development Plan.

TEHRAN, 2013, Dec. 08 -- The Chairman of the Materials and Energy Research Center Hassan Karimi said, the country will send its first home-made national communication satellite into orbit by 1397 Iranian calendar year (March 2018 - March 2019).
Karimi added that Iran’s Simorgh satellite-carrier will be sent into orbit in the spring of 2014, and noted that Sarir ultra-heavy satellite-carrier is another space project due to be launched in 1394 (March 2015 - March 2016).

If it ever exists... no design (except yours ) , no info , no unveil ( without a single launch one does not simply talk about its payload ) and if the so called sepehr is just a safir 1 with some boosters then let me tell you it can't put anything more than 200 kg into orbit.... It seems that qoqnoos is cancelled too . And i am happy if they cancel all these safir simorgh sepehr and put their energy, time and money on something practical ( maybe qaem ) with 500+ kg payload and 500+ km stable orbit .

You designed it as sepehr . right ?
View attachment 194919

My design based on simorgh with a new 2nd stage & solid strap on boosters ...

Safir-3 is the first Iranian professional carrier ...
 
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TEHRAN, 2012, March 05 -- Information by Mehdi Farahi, Director of the Aerospace Industry Organization:
Safir-2A is the first version of Safir-2 with the name of Simorgh. Length of it is 26 m, diameter of it is around 2.5 m and weight of it is around 86 tons. Thrust of is around 143 tons. It can put 100 kg satellites into 500 km altitude orbits.
The next our step is Safir-3A (Sepehr) and Safir-3B (Sarir) that can put 1,000 kg satellites into 1,000 km altitude orbits. If could add micro thrusters and some side equipments to it, it can put payloads into 36,000 km altitude orbits.
The design and production of satellite carrier rockets with a range of 1,000 kilometers are given a high priority in the country’s Five-Year Development Plan (2010-2015).
Iran aims to send other satellites into geostationary orbits, around 36,000 kilometers above the Earth's equator, after the end of the country’s Five-Year Development Plan.

TEHRAN, 2013, Dec. 08 -- The Chairman of the Materials and Energy Research Center Hassan Karimi said, the country will send its first home-made national communication satellite into orbit by 1397 Iranian calendar year (March 2018 - March 2019).
Karimi added that Iran’s Simorgh satellite-carrier will be sent into orbit in the spring of 2014, and noted that Sarir ultra-heavy satellite-carrier is another space project due to be launched in 1394 (March 2015 - March 2016).
Mate , that's fine but we are already in the fifth year ( 2015 ) ... so .. ??
 
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2 Feb:

Perigee: 231.2 km
Apogee: 476.7 km
Inclination: 55.5 °
Period: 91.5 minutes
Semi major axis: 6724 km

5 Feb:

Perigee: 229.6 km
Apogee: 463.2 km
Inclination: 55.5 °
Period: 91.3 minutes
Semi major axis: 6717 km

6 Feb:

Perigee: 228.8 km
Apogee: 447.3 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6709 km

7 Feb:

Perigee: 227.9 km
Apogee: 440.4 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6705 km

10 Feb

Perigee: 225.7 km
Apogee: 422.2 km
Inclination: 55.5 °
Period: 90.9 minutes
Semi major axis: 6694 km

11 feb

Perigee:
224.5 km
Apogee: 410.2 km
Inclination: 55.5 °
Period: 90.7 minutes
Semi major axis: 6688 km

13 feb

Perigee: 222.9 km
Apogee: 397.6 km
Inclination: 55.5 °
Period: 90.6 minutes
Semi major axis: 6681 km

15 feb
Perigee: 221.4 km
Apogee: 385.2 km
Inclination: 55.5 °
Period: 90.4 minutes
Semi major axis: 6674 km

16 feb
Perigee: 219.0 km
Apogee: 368.0 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6664 km

17 feb
Perigee: 218.0 km
Apogee: 363.9 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6661 km

Feb 20th
Perigee: 202.3 km
Apogee: 313.4 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

It's falling is becoming faster. Your prediction of its falling in two months was optimistic. ;)
 
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Feb 20th
Perigee: 202.3 km
Apogee: 313.4 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

It's falling is becoming faster. Your prediction of its falling in two months was optimistic. ;)
Yeah. I was way too optimistic. Its perigee is below 200 km now.

2 Feb:
Perigee: 231.2 km
Apogee: 476.7 km
Inclination: 55.5 °
Period: 91.5 minutes
Semi major axis: 6724 km

5 Feb:
Perigee: 229.6 km
Apogee: 463.2 km
Inclination: 55.5 °
Period: 91.3 minutes
Semi major axis: 6717 km

6 Feb:
Perigee: 228.8 km
Apogee: 447.3 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6709 km

7 Feb:
Perigee: 227.9 km
Apogee: 440.4 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6705 km

10 Feb
Perigee: 225.7 km
Apogee: 422.2 km
Inclination: 55.5 °
Period: 90.9 minutes
Semi major axis: 6694 km

11 feb
Perigee: 224.5 km
Apogee: 410.2 km
Inclination: 55.5 °
Period: 90.7 minutes
Semi major axis: 6688 km

13 feb
Perigee: 222.9 km
Apogee: 397.6 km
Inclination: 55.5 °
Period: 90.6 minutes
Semi major axis: 6681 km

15 feb
Perigee: 221.4 km
Apogee: 385.2 km
Inclination: 55.5 °
Period: 90.4 minutes
Semi major axis: 6674 km

16 feb
Perigee: 219.0 km
Apogee: 368.0 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6664 km

17 feb
Perigee: 218.0 km
Apogee: 363.9 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6661 km

18 feb
Perigee: 207.9 km
Apogee: 340.6 km
Inclination: 55.5 °
Period: 90.0 minutes
Semi major axis: 6652 km

19 feb
Perigee: 204.3 km
Apogee: 326.7 km
Inclination: 55.5 °
Period: 89.8 minutes
Semi major axis: 6643 km

20 feb
Perigee: 202.1 km
Apogee: 315.1 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

21 feb
Perigee: 198.5 km
Apogee: 301.6 km
Inclination: 55.5 °
Period: 89.5 minutes
Semi major axis: 6628 km

Welcome back :)
 
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Yeah. I was way too optimistic. Its perigee is below 200 km now.

2 Feb:
Perigee: 231.2 km
Apogee: 476.7 km
Inclination: 55.5 °
Period: 91.5 minutes
Semi major axis: 6724 km

5 Feb:
Perigee: 229.6 km
Apogee: 463.2 km
Inclination: 55.5 °
Period: 91.3 minutes
Semi major axis: 6717 km

6 Feb:
Perigee: 228.8 km
Apogee: 447.3 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6709 km

7 Feb:
Perigee: 227.9 km
Apogee: 440.4 km
Inclination: 55.5 °
Period: 91.1 minutes
Semi major axis: 6705 km

10 Feb
Perigee: 225.7 km
Apogee: 422.2 km
Inclination: 55.5 °
Period: 90.9 minutes
Semi major axis: 6694 km

11 feb
Perigee: 224.5 km
Apogee: 410.2 km
Inclination: 55.5 °
Period: 90.7 minutes
Semi major axis: 6688 km

13 feb
Perigee: 222.9 km
Apogee: 397.6 km
Inclination: 55.5 °
Period: 90.6 minutes
Semi major axis: 6681 km

15 feb
Perigee: 221.4 km
Apogee: 385.2 km
Inclination: 55.5 °
Period: 90.4 minutes
Semi major axis: 6674 km

16 feb
Perigee: 219.0 km
Apogee: 368.0 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6664 km

17 feb
Perigee: 218.0 km
Apogee: 363.9 km
Inclination: 55.5 °
Period: 90.2 minutes
Semi major axis: 6661 km

18 feb
Perigee: 207.9 km
Apogee: 340.6 km
Inclination: 55.5 °
Period: 90.0 minutes
Semi major axis: 6652 km

19 feb
Perigee: 204.3 km
Apogee: 326.7 km
Inclination: 55.5 °
Period: 89.8 minutes
Semi major axis: 6643 km

20 feb
Perigee: 202.1 km
Apogee: 315.1 km
Inclination: 55.5 °
Period: 89.7 minutes
Semi major axis: 6636 km

21 feb
Perigee: 198.5 km
Apogee: 301.6 km
Inclination: 55.5 °
Period: 89.5 minutes
Semi major axis: 6628 km

Welcome back :)
told you guys that it was falling 'fast'..

But no one seemed to care c.c
 
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U know what pathetic leech , the propellants might have failed to ignite , but this was only an experimental satellite , which is the whole point .
Why u cry and curse I really dont know. Once I heared it was launched by Safir I realized that its nothing but another toaster.

You claimed that it imagery sat, but cant show any images from it.
You claim it has endurance of 1.5 years, yet it is falling after 1 month.
Some ur friends even claimed it is 400 kg.

Sorry, but you should quit launching Safirs and move on. @SOHEIL understands that too.

Now u have 86 thanks. Enjoy. :enjoy:
 
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