Yalagach et al., 2023 - Google Patents
Configuration, design and analysis of a passive deployable mechanism for optical payloadsYalagach et al., 2023
View PDF- Document ID
- 6762683976858795842
- Author
- Yalagach A
- Gandhi R
- Honeth M
- Aglietti G
- Publication year
External Links
Snippet
The total volume of a satellite in its launch configuration is constrained by the volume available within the payload fairing of the launch vehicle. This constrains the size of the payloads on the satellite. For a high-resolution Cassegrain optical payload, there is scope to …
- 230000007246 mechanism 0 title abstract description 70
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/281—Spin-stabilised spacecraft
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Li et al. | Micro-vibration suppression methods and key technologies for high-precision space optical instruments | |
| Malbet et al. | High precision astrometry mission for the detection and characterization of nearby habitable planetary systems with the Nearby Earth Astrometric Telescope (NEAT) | |
| Menzel et al. | The design, verification, and performance of the James Webb Space Telescope | |
| Clampin | Status of the James Webb space telescope observatory | |
| Firth et al. | Minimal unpowered strain-energy deployment mechanism for rollable spacecraft booms: ground test | |
| Romualdez et al. | Overview, design, and flight results from SuperBIT: a high-resolution, wide-field, visible-to-near-UV balloon-borne astronomical telescope | |
| Dearborn et al. | A deployable membrane telescope payload for cubesats | |
| Zhang et al. | Space advanced technology demonstration satellite | |
| Yalagach et al. | Configuration, design and analysis of a passive deployable mechanism for optical payloads | |
| Honeth et al. | Wire driven mechanisms for deployable components for optical payloads | |
| Lillie | Large deployable telescopes for future space observatories | |
| Rafanelli et al. | Revolutionary astrophysics using an incoherent synthetic optical aperture | |
| Lee et al. | Space interferometry mission spacecraft pointing error budgets | |
| Yalagach et al. | Deployable barrel for a cubesat's optical payload | |
| Brugarolas et al. | ACCESS pointing control system | |
| Malbet et al. | NEAT: a spaceborne astrometric mission for the detection and characterization of nearby habitable planetary systems | |
| Sato et al. | Extensible flexible optical system for nano-scale remote sensing satellite “PRISM” | |
| Yalagach et al. | Parametrization and Practical Implementation of Deployable Optical Systems | |
| Lillie et al. | Adaptation in space telescopes | |
| Bronowicki | Forensic investigation of reaction wheel nutation on isolator | |
| De Maeyer et al. | 4U DEPLOYABLE TELESCOPE FOR SMALLSATS | |
| Li et al. | Practical strategies to stabilize a nanosatellite platform with a space camera and integrated mechanical parts | |
| Angel et al. | Extremely large space telescopes and interferometers made with flat primary mirrors | |
| Kapoor et al. | Design & development of X-ray Solar Monitor (XSM) filter wheel drive mechanism with self hold down feature for chandrayaan-2 orbiter | |
| Madsen et al. | The extendable boom and laser metrology design for the high energy x-ray probe (HEX-P) |