AU2009100967A4 - Space Delivery Vehicle - Google Patents
Space Delivery Vehicle Download PDFInfo
- 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
Links
- 239000003562 lightweight material Substances 0.000 claims description 3
- 235000015842 Hesperis Nutrition 0.000 claims 2
- 235000012633 Iberis amara Nutrition 0.000 claims 2
- 239000000463 material Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 1
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 239000002760 rocket fuel Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
- B64B1/30—Arrangement of propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
- B64G1/005—Air 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.
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)
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 |
-
2009
- 2009-09-23 AU AU2009100967A patent/AU2009100967A4/en not_active Ceased
Cited By (9)
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 |