计划中的安加拉7型火箭！！

赫鲁尼切夫开始计划安加拉系列的新型号！这就是高粱陈君所想要的中等运力火箭！！
Detailed information about Angara-7 was first published around 2006, however it is apparent that planners at Khrunichev enterprise had started working on the concept sometimes earlier. If ever built, the Angara-7 would double the payload capacity of Russia contemporary heavy lifter -- the Proton rocket. Unlike all previous versions of the Angara family of launchers, the Angara-7 would feature a central core module with the diamater inherited from Proton. Six standard rocket modules, known by their Russian abbreviation -- URM for Universalniy Raketniy Modul -- borrowed from previous Angara rockets would comprise the first stage.

As in all other members of the Angara family, all booster stages of the rocket would be equipped with the RD-191 engine, however, it appeared from the orginal drawings that the engine on the central core stage would feature a nozzle extension, designed to optimize its performance beyond the Earth atmosphere. (316)

The Angara-7 concept was further refined by May 2008, when two variations of the vehicle, known as Angara-7P and Angara-7V, had been revealed at the 1st Joint Conference "Space for Humanity." (The event was organized by Tsiolkovsky Russian Academy of Cosmonautics and the International Astronautics Academy).

The "7P" version, where "P" stands for "pilotiruemaya" (piloted) could potentially compete in the government tender for the development of the next-generation rocket of the manned space program. The vehicle would fly from a yet-to-be-built Vostochny center in the Russian Far East.

The May 2008 depictions of the Angara-7 appeared to show nozzle extensions on all RD-191 engines of the first and second stage.

Along with booster stages, Khrunichev enterprise revealed concepts of three high-performance upper stages, burning liquid hydrogen and liquid oxygen. One of those stages -- KVRB -- would be "customized" for the Angara-7V rocket, where "V" stands for "vodorod" (hydrogen).赫鲁尼切夫开始计划安加拉系列的新型号！这就是高粱陈君所想要的中等运力火箭！！
Detailed information about Angara-7 was first published around 2006, however it is apparent that planners at Khrunichev enterprise had started working on the concept sometimes earlier. If ever built, the Angara-7 would double the payload capacity of Russia contemporary heavy lifter -- the Proton rocket. Unlike all previous versions of the Angara family of launchers, the Angara-7 would feature a central core module with the diamater inherited from Proton. Six standard rocket modules, known by their Russian abbreviation -- URM for Universalniy Raketniy Modul -- borrowed from previous Angara rockets would comprise the first stage.

As in all other members of the Angara family, all booster stages of the rocket would be equipped with the RD-191 engine, however, it appeared from the orginal drawings that the engine on the central core stage would feature a nozzle extension, designed to optimize its performance beyond the Earth atmosphere. (316)

The Angara-7 concept was further refined by May 2008, when two variations of the vehicle, known as Angara-7P and Angara-7V, had been revealed at the 1st Joint Conference "Space for Humanity." (The event was organized by Tsiolkovsky Russian Academy of Cosmonautics and the International Astronautics Academy).

The "7P" version, where "P" stands for "pilotiruemaya" (piloted) could potentially compete in the government tender for the development of the next-generation rocket of the manned space program. The vehicle would fly from a yet-to-be-built Vostochny center in the Russian Far East.

The May 2008 depictions of the Angara-7 appeared to show nozzle extensions on all RD-191 engines of the first and second stage.

Along with booster stages, Khrunichev enterprise revealed concepts of three high-performance upper stages, burning liquid hydrogen and liquid oxygen. One of those stages -- KVRB -- would be "customized" for the Angara-7V rocket, where "V" stands for "vodorod" (hydrogen).