Jupiter III Booster Separation
Team Vision 2006 Proposal
An Alternate Approach towards Achieving the New Vision
for Space Exploration
The Jupiter-III HLV is a revolutionary idea that seeks to revamp the current External Tank/SRB system of the Space Shuttle to produce a cutting-edge heavy lift launch vehicle. This proposal involves replacing the forward attachment of the External Tank with a more formidable structural system, thereby enhancing the capacity to transmit higher thrust and rotational loads. The new center tank's upper inter-stage region would drive the attached External Tank/SRB components, reducing the stress on the aft attachment points of the LH2 tanks.
This HLV concept leverages the External Tank/SRB stack as a common core booster, providing ample room for adjustments in lift capacity through modifications to the central core lift vehicle. The parallel burn configuration of the Jupiter-III HLV offers numerous advantages, including a reduction in development costs, improved structural efficiency, and heightened payload capacity flexibility. With a large proportion of already developed components in the Shuttle External Tank/SRB system, the costs of developing this HLV would be kept to a minimum.
Moreover, the Jupiter-III HLV would optimally utilize the Kennedy Spaceflight Center's Vehicle Assembly Building (VAB) volume, making it a more practical option than conventional stacked lift vehicle designs. With further extensions to a four SSET Jupiter V configuration integrated around a new 14 Meter ICES core and main/2nd stage engines, the lift capacity of this HLV could potentially surpass 1,000 metric tons to low Earth orbit, making it a game-changer in the aerospace industry.
Music: http://www.purple-planet.com
#spaceshuttle #nasa #ksp
Видео Jupiter III Booster Separation канала Hazegrayart
An Alternate Approach towards Achieving the New Vision
for Space Exploration
The Jupiter-III HLV is a revolutionary idea that seeks to revamp the current External Tank/SRB system of the Space Shuttle to produce a cutting-edge heavy lift launch vehicle. This proposal involves replacing the forward attachment of the External Tank with a more formidable structural system, thereby enhancing the capacity to transmit higher thrust and rotational loads. The new center tank's upper inter-stage region would drive the attached External Tank/SRB components, reducing the stress on the aft attachment points of the LH2 tanks.
This HLV concept leverages the External Tank/SRB stack as a common core booster, providing ample room for adjustments in lift capacity through modifications to the central core lift vehicle. The parallel burn configuration of the Jupiter-III HLV offers numerous advantages, including a reduction in development costs, improved structural efficiency, and heightened payload capacity flexibility. With a large proportion of already developed components in the Shuttle External Tank/SRB system, the costs of developing this HLV would be kept to a minimum.
Moreover, the Jupiter-III HLV would optimally utilize the Kennedy Spaceflight Center's Vehicle Assembly Building (VAB) volume, making it a more practical option than conventional stacked lift vehicle designs. With further extensions to a four SSET Jupiter V configuration integrated around a new 14 Meter ICES core and main/2nd stage engines, the lift capacity of this HLV could potentially surpass 1,000 metric tons to low Earth orbit, making it a game-changer in the aerospace industry.
Music: http://www.purple-planet.com
#spaceshuttle #nasa #ksp
Видео Jupiter III Booster Separation канала Hazegrayart
Показать
Комментарии отсутствуют
Информация о видео
Другие видео канала
![Apollo Command and Service Module Shuttle](https://i.ytimg.com/vi/xox-yQADUTM/default.jpg)
![Falcon9](https://i.ytimg.com/vi/hq5nWrjH9HI/default.jpg)
![Von Braun's Lunar Lander Moon Landing](https://i.ytimg.com/vi/ZXv4fLrpfnI/default.jpg)
![National Launch System Heavy Lift Vehicle with Energia Boosters](https://i.ytimg.com/vi/-8f7QMGCgew/default.jpg)
![Energia Vulkan Moon Rocket](https://i.ytimg.com/vi/-r7pb17EQ60/default.jpg)
![Rocket Lab's Reusable Neutron Rocket Animation](https://i.ytimg.com/vi/bsUxlVh6b8Q/default.jpg)
![Apollo 12: The Second Moonwalk - Pete Conrad and Alan Bean's historic lunar journey](https://i.ytimg.com/vi/-bACGSOMMVg/default.jpg)
![NASA's Shuttle-Derived Heavy Lift Launch Vehicle Concept](https://i.ytimg.com/vi/Il4xDpx4rJk/default.jpg)
![How To Get Your Hypersonic Lifting Body To Space: Featuring The FDL-5](https://i.ytimg.com/vi/0EUHgRBJkf4/default.jpg)
![NASA's Unpressurized Lunar Lander](https://i.ytimg.com/vi/_ArHsCeijzM/default.jpg)
![Philip Bono's Reusable Single Stage to Orbit Rocket (SSTO)](https://i.ytimg.com/vi/YfvG0v1LX6k/default.jpg)
![Boeing Rocket Concepts](https://i.ytimg.com/vi/4Kk9CWegvxQ/default.jpg)
![ESA's Airbus Reusable Rocket: The Adeline](https://i.ytimg.com/vi/5VFolmVAuYk/default.jpg)
![Apollo 11 Moonbound pt1](https://i.ytimg.com/vi/VS3sHWFDZuo/default.jpg)
![What Will Our Moon Look Like in the Future](https://i.ytimg.com/vi/orlDDYVaNzg/default.jpg)
![NASA's DART Spacecraft Hitting an Asteroid Headed by Earth at 6.6 kilometers per second simulation](https://i.ytimg.com/vi/zJesYqtEWeQ/default.jpg)
![Moon South Pole 2055](https://i.ytimg.com/vi/WD6UNQCDXE4/default.jpg)
![TWA Moonliner: Early Civilian Space Flight Rocket](https://i.ytimg.com/vi/UYvLldk-zIg/default.jpg)
![Langley Unpressurized Lunar Lander](https://i.ytimg.com/vi/M0myjsdQ-ng/default.jpg)
![The Methane Rocket Revolution is Here](https://i.ytimg.com/vi/aNGhdKqU0Aw/default.jpg)
![HOTOL Britain's Air Breathing SSTO Spaceplane Rocket](https://i.ytimg.com/vi/bpdJtE4Sl7U/default.jpg)