Bhat et al., 2011 - Google Patents
Design of a Payload Recovery Device in case of accidental breakage of tether of an aerostatBhat et al., 2011
- Document ID
- 15395467797416786004
- Author
- Bhat C
- Pant R
- Publication year
- Publication venue
- 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference, including the AIAA Balloon Systems Conference and 19th AIAA Lighter-Than
External Links
Snippet
An Aerostat is an aerodynamically shaped envelope filled with a Lighter-Than-Air (LTA) gas and tethered to the ground. It can be used as an aerial platform to carry payloads for several applications such as surveillance and photography. One of the main operational problems …
- 238000011084 recovery 0 title abstract description 9
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
-
- 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
- B64B1/32—Arrangement of propellers surrounding hull
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20170029111A1 (en) | Unmanned aerial vehicle and method for launching | |
Smith et al. | Applications of scientific ballooning technology to high altitude airships | |
US20150183520A1 (en) | Unmanned aerial vehicle and method for launching | |
CN115057015A (en) | Method for manufacturing high microgravity environment by using high microgravity scientific experimental device | |
Mahmood et al. | Tethered aerostat envelope design and applications: A review | |
Bhat et al. | Design of a Payload Recovery Device in case of accidental breakage of tether of an aerostat | |
Jones et al. | Solar montgolfiere balloons for Mars | |
Smith et al. | The hisentinel airship | |
Aaron et al. | A method for balloon trajectory control | |
Aaron et al. | Balloon trajectory control | |
Dorrington | Concept options for the aerial survey of Titan | |
Izraelevitz et al. | Subscale prototype and hangar test flight of a Venus variable-altitude aerobot | |
Jacob et al. | Solar balloon development for high altitude observations | |
CN208264545U (en) | floating device | |
Sóbester et al. | Notes on meteorological balloon mission planning | |
Sharma et al. | Design and Field Trials of a Payload Recovery Device for Tethered Aerostats | |
US20210061436A1 (en) | Flight termination system for aerial vehicles | |
Schuler et al. | Solar high altitude balloons as a long duration controllable aerial platform | |
Schuler et al. | Altitude Control with Vented Solar High Altitude Balloons (SHAB-Vs) | |
Mallesh et al. | Numerical Analysis of a PRD for a Tethered Lighter than Air Vehicle | |
Hough | Design and Operations of Multi-Hour Stratospheric Solar Hot-Air Balloons | |
Karna | Designing a Rocket-Balloon Hybrid Launch System for Affordable Access to Suborbital Space | |
US11208191B2 (en) | Flight termination system for tethered aerial vehicles | |
Dunker et al. | Guided Parafoil High Altitude Research (GPHAR) Flight at 57,122 ft | |
Ben-Ora et al. | Design and Flight of an Autonomous Rogallo Glider for Recovery of High-Altitude Balloon Payloads and Data |