AU2009100967A4 - Space Delivery Vehicle - Google Patents

Space Delivery Vehicle Download PDF

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Publication number
AU2009100967A4
AU2009100967A4 AU2009100967A AU2009100967A AU2009100967A4 AU 2009100967 A4 AU2009100967 A4 AU 2009100967A4 AU 2009100967 A AU2009100967 A AU 2009100967A AU 2009100967 A AU2009100967 A AU 2009100967A AU 2009100967 A4 AU2009100967 A4 AU 2009100967A4
Authority
AU
Australia
Prior art keywords
air
vehicle
space
atmosphere
structures
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
AU2009100967A
Inventor
Gaffar A. Khan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to AU2009100967A priority Critical patent/AU2009100967A4/en
Application granted granted Critical
Publication of AU2009100967A4 publication Critical patent/AU2009100967A4/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D5/00Aircraft transported by aircraft, e.g. for release or reberthing during flight
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/06Rigid airships; Semi-rigid airships
    • B64B1/24Arrangement of propulsion plant
    • B64B1/30Arrangement of propellers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/002Launch systems
    • B64G1/005Air launch

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Remote Sensing (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Description

Description Figure #1. Part # 1: Rocket boosters to navigate back to earth's atmosphere once in space. Figure #1. Part # 2: Huge hollow stable structures emptied of its air and its pressure controlled through the structure (part #3) and onboard compressors(part # 4) and pilot (part # 5). Figure #1. Part # 3: Huge structure to hold hollow spherical stable structures and control its air pressure. Figure #1. Part # 4: Onboard air compressor and pressure units. Figure #1. Part # 5: Chamber for pilot and control equipments. Figure #1. Part # 6: Onboard propulsion system to navigate in lower atmosphere once closer to ground Figure #1. Part # 7: Payload, or cargo or space travel vehicle or rocket or satellites which are meant to dropped or delivered in space. Principle behind the construction and operation of this vehicle: (Part #2) Huge hollow stable structures are built strong enough to withstand sea level atmospheric pressure. And all the air from it is be pumped out. These hollow structures are designed in spherical shape, as, spheres are the only shapes whose surface area and volume ratio is the least when compared with other shapes. So, least consumption of material and maximum volume of air that can be removed is achieved. The weight of the air is approximately 1.2 kg / cubic meter, So, the total weight of material used to construct the hollow stable structure used is very much less than the weight of the volume of air pumped out of the structure. In that situation the hollow structure will float in the air. The total material weight of the hollow structure with no air in it should be < (the weight of the volume of air pumped out + the payload). At that stage this sphere will automatically ascend into space as per Archimedes principle. The construction of these huge hollow stable structure is done by means of block of very light weight material.
However, bringing back this sphere safely back to earth on its designated location would not be easy. In order to address this issue, a huge structure of light weight material is constructed (Part# 3) connecting many such hollow structures to achieve more weight lifting capacity, and control of its pressure. The main purpose of this structure is to: 1. Hold together all the individual spherical structures together 2. To bring back all the sphere to earth 3. To increase the payload capacity to a much higher fold, All spherical structures (Part# 2) are connected in a huge ring shaped structure (Part# 3) whose diameter can be imagined to be around 3 of a km or so. In this way, many such spherical structures are connected and controlled through a huge ring and control the air pressure of the sphere through the ring structure, a pilot cabin(Part# 5). This cabin is constructed to withstand conditions of different altitude of atmosphere and the conditions of space. (Part# 4) is a onboard air compressor and monitor & control system. (Part# 6) is a propeller to do little navigation of the entire system once back into atmosphere and closer to ground. In this way the system can be reused again and again to go and come back from space. Operation: On the ground these hollow spherical structures (Part# 2) are vacuumed to get a lift off. Once on the atmosphere or in space reaching a suitable height, the payload or satellite or space vehicle or rocket is released to navigate itself by its own propulsion system. Using the onboard booster (Part # 1). The vehicle is guided back to earth's atmosphere by the pilot onboard (Part #5) if its drifted into space. Once in atmosphere the spherical structures are refilled with air slowly to make a slow descend down to earth due to the weight of the air in it. The speed of the vehicle is controlled by the pumping out air from the spherical structures by the onboard compressor unit (Part # 4). Free fall into earth due to gravity is thus avoided to prevent air friction. The speed of the entire system can be controlled by the pilot using air compressor to do slow descend. Once close enough to ground using propellers (Part # 6) vehicle is landed to its required base. Conclusion: A huge cost of burning expensive rocket fuel to get upward is thus avoided by using this vehicle. The vehicle is reusable and safe.

Claims (4)

1. Reusable delivery vehicle to deliver rockets, or satellites or cargo payloads or space travel vehicles to space or atmosphere by using a collection of hollow stable structures which weigh lesser than the air they can contain by means of very low pressure to nil pressure, manoeuvred by manned/ controlled rocket or propulsion system to drop satellites/ rockets/ payloads /space travel vehicle in to space.
2. Achievement of upward lift and weight lifting capacity by means of single or multiple huge hollow stable structures emptied of its air to vacuum and its air pressure controlled. Huge hollow stable structures are constructed with very light weight material and the structure is air proof.
3. Re-entry of the vehicle into earth's atmosphere by means onboard rocket boosters after the delivery mission by the pilot. And slow descend to earth by means of filling hollow stable structures with air to make a slower descend to avoid free fall upon re-entry into atmosphere, by means of controlling pressure inside the structures.
4. Upon re-entry into lower altitude, manoeuvring of vehicle using onboard propeller system operated by the pilot to its destination safely.
AU2009100967A 2009-09-23 2009-09-23 Space Delivery Vehicle Ceased AU2009100967A4 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2009100967A AU2009100967A4 (en) 2009-09-23 2009-09-23 Space Delivery Vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AU2009100967A AU2009100967A4 (en) 2009-09-23 2009-09-23 Space Delivery Vehicle

Publications (1)

Publication Number Publication Date
AU2009100967A4 true AU2009100967A4 (en) 2009-11-05

Family

ID=41259271

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2009100967A Ceased AU2009100967A4 (en) 2009-09-23 2009-09-23 Space Delivery Vehicle

Country Status (1)

Country Link
AU (1) AU2009100967A4 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2394489A1 (en) * 2010-09-27 2013-02-01 Fundacion Centauri Multi-eye space vehicle transfer to low terrestrial orbit (Machine-translation by Google Translate, not legally binding)
WO2014094712A2 (en) * 2012-12-20 2014-06-26 Astrium Gmbh Auxiliary device for high-flying aircraft
WO2016167733A1 (en) * 2015-04-17 2016-10-20 Eroğlu Ali Riza Acquisition and landing systems of airscrafts and spacecrafts in air and space
EP3480106A1 (en) * 2017-09-29 2019-05-08 Ludovico Turinetti Vacuum airship made from individual elements
US20220127017A1 (en) * 2019-03-21 2022-04-28 Szabolcs TAKÁCS A floating platform for launching a space rocket from a height and method for launching a rigid -walled balloon into the space

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2394489A1 (en) * 2010-09-27 2013-02-01 Fundacion Centauri Multi-eye space vehicle transfer to low terrestrial orbit (Machine-translation by Google Translate, not legally binding)
WO2014094712A2 (en) * 2012-12-20 2014-06-26 Astrium Gmbh Auxiliary device for high-flying aircraft
WO2014094712A3 (en) * 2012-12-20 2014-09-04 Astrium Gmbh Auxiliary device for high-flying aircraft
CN105026262A (en) * 2012-12-20 2015-11-04 空中客车防卫和太空有限责任公司 Auxiliary device for high-flying aircraft
JP2016501162A (en) * 2012-12-20 2016-01-18 エアバス ディフェンス アンド スペース ゲーエムベーハーAirbus Defence and Space GmbH Auxiliary device for high altitude flying object
AU2013362361B2 (en) * 2012-12-20 2017-07-06 Airbus Defence and Space GmbH Auxiliary device for high-flying aircraft
WO2016167733A1 (en) * 2015-04-17 2016-10-20 Eroğlu Ali Riza Acquisition and landing systems of airscrafts and spacecrafts in air and space
EP3480106A1 (en) * 2017-09-29 2019-05-08 Ludovico Turinetti Vacuum airship made from individual elements
US20220127017A1 (en) * 2019-03-21 2022-04-28 Szabolcs TAKÁCS A floating platform for launching a space rocket from a height and method for launching a rigid -walled balloon into the space

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Legal Events

Date Code Title Description
FGI Letters patent sealed or granted (innovation patent)
MK22 Patent ceased section 143a(d), or expired - non payment of renewal fee or expiry