RU2016103558A - An aviation rocket and space complex, formed on the basis of a space rocket adapted from the TOPOL-M ICBM and the IL-76MF carrier aircraft to launch small spacecraft into target orbits, by landing the ILV from the aircraft using a combined launch and loading and stabilizing platform parachute - Google Patents

An aviation rocket and space complex, formed on the basis of a space rocket adapted from the TOPOL-M ICBM and the IL-76MF carrier aircraft to launch small spacecraft into target orbits, by landing the ILV from the aircraft using a combined launch and loading and stabilizing platform parachute Download PDF

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RU2016103558A
RU2016103558A RU2016103558A RU2016103558A RU2016103558A RU 2016103558 A RU2016103558 A RU 2016103558A RU 2016103558 A RU2016103558 A RU 2016103558A RU 2016103558 A RU2016103558 A RU 2016103558A RU 2016103558 A RU2016103558 A RU 2016103558A
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Russia
Prior art keywords
rocket
launch
landing
complex
space
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RU2016103558A
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Russian (ru)
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RU2636447C2 (en
Inventor
Михаил Маркович Ковалевский
Юрий Геннадьевич Мехоношин
Владимир Николаевич Чижухин
Сергей Владимирович Чижухин
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Владимир Николаевич Чижухин
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Claims (1)

Авиационный ракетно-космический комплекс (АРКК) по выведению малых КА весом до 1000 кг на орбиты с высотой до 1500 км на базе РКН с ЖРД, десантируемой из фюзеляжа СН АН-124-100 с применением «минометного» старта из транспортно-пускового контейнера, отличающийся тем, что, с целью исключения из состава ракетного сегмента на борту СН сложных технических систем обслуживания РКН, размещенных в транспортно-пусковом контейнере с комплексом «минометного» десантирования РКН, для формирования АРКК применяется твердотопливная РКН на базе утилизируемой МБР «Тополь-М» и штатный военно-транспортный СН ИЛ-76МФ, благоприятное сочетание весогабаритных и энергетических параметров которых, обеспечивают реализацию подготовки к запуску и десантирование РКН с облегченной транспортно-пусковой платформы с применением комплекса парашютных систем на базе подъемно-стабилизирующего парашюта, обеспечивающих оптимальные массово-габаритные параметры ракетного сегмента, с сохранением штатных условий эксплуатации РКН и СН и необходимые начальные условия безопасного проведения режима десантирования для экипажа самолета при последующем запуске двигателя первой ступени РКН.Aviation Rocket and Space Complex (ARKK) for launching small spacecraft with a weight of up to 1000 kg into orbits with a height of up to 1500 km on the basis of a rocket launcher with a rocket engine landing from the fuselage SN AN-124-100 using a "mortar" launch from a transport and launch container, characterized in that, in order to exclude from the composition of the missile segment aboard the missile launcher complex technical service systems for rocket launchers located in a transport-launch container with a mortar landing complex for rocket launchers, solid rocket launchers based on the utilized MB are used to form the ARCC "Topol-M" and the standard military transport SN IL-76MF, the favorable combination of weight and energy parameters of which provide preparation for launch and landing of the rocket launcher from a lightened transport and launch platform using a complex of parachute systems based on a lifting and stabilizing parachute, providing the optimal mass and dimensional parameters of the rocket segment, while maintaining the normal operating conditions of the rocket and rocket launchers and the necessary initial conditions for the safe conduct of the landing mode for I am the crew of the aircraft during the subsequent engine start of the first stage of the ILV.
RU2016103558A 2016-02-04 2016-02-04 Aircraft rocket launch site formed on basis of space-mission vehicle adapted from topol-m icbm and carrier aircraft il-76mf for insertion of small spacecrafts into final orbits by inserting smv from aircraft using combined transport-launching platform and lifting-stabilizing parachute RU2636447C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016103558A RU2636447C2 (en) 2016-02-04 2016-02-04 Aircraft rocket launch site formed on basis of space-mission vehicle adapted from topol-m icbm and carrier aircraft il-76mf for insertion of small spacecrafts into final orbits by inserting smv from aircraft using combined transport-launching platform and lifting-stabilizing parachute

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016103558A RU2636447C2 (en) 2016-02-04 2016-02-04 Aircraft rocket launch site formed on basis of space-mission vehicle adapted from topol-m icbm and carrier aircraft il-76mf for insertion of small spacecrafts into final orbits by inserting smv from aircraft using combined transport-launching platform and lifting-stabilizing parachute

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RU2016103558A true RU2016103558A (en) 2017-08-10
RU2636447C2 RU2636447C2 (en) 2017-11-23

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RU2016103558A RU2636447C2 (en) 2016-02-04 2016-02-04 Aircraft rocket launch site formed on basis of space-mission vehicle adapted from topol-m icbm and carrier aircraft il-76mf for insertion of small spacecrafts into final orbits by inserting smv from aircraft using combined transport-launching platform and lifting-stabilizing parachute

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Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4901949A (en) * 1988-03-11 1990-02-20 Orbital Sciences Corporation Ii Rocket-powered, air-deployed, lift-assisted booster vehicle for orbital, supraorbital and suborbital flight
US5740985A (en) * 1996-09-16 1998-04-21 Scott; Harry Low earth orbit payload launch system
RU2160215C1 (en) * 1999-07-29 2000-12-10 Карпов Анатолий Степанович Aero-space system
RU2549923C2 (en) * 2013-02-07 2015-05-10 Закрытое акционерное общество "Научно-внедренческий центр "Атмосфера" Method of launching carrier rocket from aircraft with help of lifting-stabilising parachute

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20190205