Information about Start-1 ICBM Conversion Rocket Family

[osiossim]

Does anybody have concreate information about Start-1 launcher? Despite its limited lift-off capacity, I would expect many small satellite manufacturers turn their face to Start-1, in stead of problematic Dnepr.

But Start-1 seems so slient even if they will launch Eros-C in 2009.

[VDD1991]

Info and specs about the Start-1 rocket are available at this link:

https://en.wikipedia.org/wiki/Start-1

[owais.usmani]

https://tass.ru/kosmos/17514141

Launch vehicle "Start-1M" will be created in Russia

MOSCOW, 13 April. /TASS/. The Start-1M conversion launch vehicle was developed in the Russian Federation, its model was first presented at the Sphere congress, a TASS correspondent reports on Thursday from the scene.

According to the information presented at the stand of the Agat organization, the developer is the Moscow Institute of Thermal Engineering (part of Roscosmos). "The complex provides for the preparation and launch of spacecraft (spacecraft - TASS note) weighing 150-700 kg into orbits with an altitude of 200-1,500 km from the Vostochny and Plesetsk cosmodromes," the organization's materials say.

It is clarified that the advantages of the complex are the high efficiency of removing the load, the low cost of the rocket, increased reliability, and the ability to use the existing infrastructure.

"JSC" Organization "Agat" took part in the assessment of the economic efficiency of the use of the complex," the materials say.