gardnerdesign
New Member
My design is for an airborne expeditionary vehicle that will initially be capable of precision airdrop, with the future capability of being integrated with a variety of lift surfaces and airborne propulsion systems. This vehicle will integrate aerodynamic properties into its design, while still retaining the ability to be resistant to small arms fire and artillery fragmentation. The vehicle will be produced in a 4X4, 6X6, and 8X8 variant that will be equipped with a modular payload section to perform a variety of battlefield functions.The target weights for all variants of the vehicle will be between 8-12 tons. The vehicle will be capable of operating autonomously as an unmanned ground vehicle, this feature will allow for vehicles to be sent in to areas were there is low situational awareness and a high risk of enemy engagement. The ability to act as a UGV means that if carrying troops ounce dismounted the vehicle can support the dismounted troops without risking the life of a driver or a weapons operator. When equipped with a manned payload section the vehicle will be capable of control via an onboard or dismounted soldier (if desired) as well as retaining its autonomous operational capability.
An example of how the vehicle will be most commonly be utilized is as follows: one to four vehicles (depending on variant and transport size) will be loaded onto a transport with 0-8 men in each vehicle (depending on variant) and flown into a potential war zone. Once over the battlefield, the vehicles will be ejected from the rear of the transport and will utilize their aerodynamic bodies and a deployable Para foil to precisely land at predetermined landing zones. Or in the case of standoff variants, it will utilize its control surfaces ounce released to silently glide into the war zone and will land softly utilizing retro rockets. If carrying troops, they will then immediately dismount and operate on foot while the vehicle becomes an unmanned ground vehicle and provides supporting fire and long range ground mobility when needed. As the design progresses and lifting and propulsion systems are integrated, the vehicle will fly itself into a war zone. Upon landing wings or rotors would fold towards the body so that they will not be damaged or hinder the movement of the vehicle on the ground. If carrying troops, the troops would dismount and be supported by the vehicle. When redeployment becomes necessary they will board the vehicle and fly to the next landing zone.
Key features of the vehicle will include: An aerodynamic body to increase speed range and accuracy during airdrop as well as being a key component in the integration of flight capabilities. In-rim electric engines to save space onboard the vehicles body, as well as improving survivability. Pneumatic shock absorbers that allow for increased ground mobility, and also allow the vehicle to improve its aerodynamics by folding in its wheels and stowing them. A hybrid propulsion system to provide fuel-efficient ground mobility. A modular payload section that allows the vehicle to operate as an IFV, APC, mobile command center, ambulance, logistics vehicle or any other necessitated function. The vehicle will also include a powerful central computer that can perform the necessary computations for autonomous ground and flight operation as well as all necessitated combat computations, such as, target acquisition, firing solutions, command and communication functions etc.
The bottom half of the vehicle will be the base unit comprising of the vehicles ground mobility systems and computer core. The computer core will be contained in an extremely well armored housing, able to withstand even the heaviest IED as well as being resistant to the temperatures encountered in a vehicle that is on fire. The ground mobility system will include fuel tanks and batteries for storing energy as well as a generator for converting chemical energy into electric energy to be stored by the batteries. A pneumatic shock system will allow the vehicle to traverse very rough terrain and insure that the best traction possible is achieved by keeping as many wheels on the ground as possible. In-rim electric engines in all wheels will provide the ground mobility and range necessary to make the vehicle successful. In addition electric motors provide higher torque necessary for navigating rough and mountainous terrain. By incorporating the electric engines in the rim of all wheels on the vehicle you not only save space and weight but u drastically improve the survivability of a vehicle, in the event of one or more engines or wheels being disabled the vehicle will still retain enough mobility to retreat or fight on. This section will also include space within the body to allow for the wheels to be folded in and stowed to reduce drag and increase aerodynamic efficiency.
The top half of the vehicle is the modular payload section and will come in many different variants allowing the vehicle to fill various battlefield functions. This section will contain all primary sensors and airborne capabilities, such as lifting surfaces, control surfaces, Para foil, or propulsion systems. The payload section can be fitted with various weapons or equipment to allow the vehicle to fulfill combat support roles. The payload section can be designed to allow for troop accommodations in the infantry-fighting vehicle or armored troop carrying variants. The emphases on modular design reduces development cost while vastly improving operational capability. It allows a vehicle to be easily retrofitted with new equipment, as well as giving it the novel capability of being able to quickly adapt to changing battlefield needs.
The vehicles aerodynamic design allows for future integration of airmobile propulsion systems such as, counter-rotating helicopter blades, folding wings with tilt rotors, folding wings with jet engines and folding wings with air-augmented rockets. This will provide the capability to not only deploy support vehicles and troops by air but also quickly redeploy them by air. The vehicle can also be equipped with just lifting surfaces and can act as a glider to give the vehicle a standoff precision airdrop capability. The integration of these features will allow for the first time in military history an air transportation system to be integrated with the vehicle it is intended to transport. This capability allows for future air-mechanization tactics and strategy to be utilized to their full potential.
An example of how the vehicle will be most commonly be utilized is as follows: one to four vehicles (depending on variant and transport size) will be loaded onto a transport with 0-8 men in each vehicle (depending on variant) and flown into a potential war zone. Once over the battlefield, the vehicles will be ejected from the rear of the transport and will utilize their aerodynamic bodies and a deployable Para foil to precisely land at predetermined landing zones. Or in the case of standoff variants, it will utilize its control surfaces ounce released to silently glide into the war zone and will land softly utilizing retro rockets. If carrying troops, they will then immediately dismount and operate on foot while the vehicle becomes an unmanned ground vehicle and provides supporting fire and long range ground mobility when needed. As the design progresses and lifting and propulsion systems are integrated, the vehicle will fly itself into a war zone. Upon landing wings or rotors would fold towards the body so that they will not be damaged or hinder the movement of the vehicle on the ground. If carrying troops, the troops would dismount and be supported by the vehicle. When redeployment becomes necessary they will board the vehicle and fly to the next landing zone.
Key features of the vehicle will include: An aerodynamic body to increase speed range and accuracy during airdrop as well as being a key component in the integration of flight capabilities. In-rim electric engines to save space onboard the vehicles body, as well as improving survivability. Pneumatic shock absorbers that allow for increased ground mobility, and also allow the vehicle to improve its aerodynamics by folding in its wheels and stowing them. A hybrid propulsion system to provide fuel-efficient ground mobility. A modular payload section that allows the vehicle to operate as an IFV, APC, mobile command center, ambulance, logistics vehicle or any other necessitated function. The vehicle will also include a powerful central computer that can perform the necessary computations for autonomous ground and flight operation as well as all necessitated combat computations, such as, target acquisition, firing solutions, command and communication functions etc.
The bottom half of the vehicle will be the base unit comprising of the vehicles ground mobility systems and computer core. The computer core will be contained in an extremely well armored housing, able to withstand even the heaviest IED as well as being resistant to the temperatures encountered in a vehicle that is on fire. The ground mobility system will include fuel tanks and batteries for storing energy as well as a generator for converting chemical energy into electric energy to be stored by the batteries. A pneumatic shock system will allow the vehicle to traverse very rough terrain and insure that the best traction possible is achieved by keeping as many wheels on the ground as possible. In-rim electric engines in all wheels will provide the ground mobility and range necessary to make the vehicle successful. In addition electric motors provide higher torque necessary for navigating rough and mountainous terrain. By incorporating the electric engines in the rim of all wheels on the vehicle you not only save space and weight but u drastically improve the survivability of a vehicle, in the event of one or more engines or wheels being disabled the vehicle will still retain enough mobility to retreat or fight on. This section will also include space within the body to allow for the wheels to be folded in and stowed to reduce drag and increase aerodynamic efficiency.
The top half of the vehicle is the modular payload section and will come in many different variants allowing the vehicle to fill various battlefield functions. This section will contain all primary sensors and airborne capabilities, such as lifting surfaces, control surfaces, Para foil, or propulsion systems. The payload section can be fitted with various weapons or equipment to allow the vehicle to fulfill combat support roles. The payload section can be designed to allow for troop accommodations in the infantry-fighting vehicle or armored troop carrying variants. The emphases on modular design reduces development cost while vastly improving operational capability. It allows a vehicle to be easily retrofitted with new equipment, as well as giving it the novel capability of being able to quickly adapt to changing battlefield needs.
The vehicles aerodynamic design allows for future integration of airmobile propulsion systems such as, counter-rotating helicopter blades, folding wings with tilt rotors, folding wings with jet engines and folding wings with air-augmented rockets. This will provide the capability to not only deploy support vehicles and troops by air but also quickly redeploy them by air. The vehicle can also be equipped with just lifting surfaces and can act as a glider to give the vehicle a standoff precision airdrop capability. The integration of these features will allow for the first time in military history an air transportation system to be integrated with the vehicle it is intended to transport. This capability allows for future air-mechanization tactics and strategy to be utilized to their full potential.