Mikulas Jr et al., 1989 - Google Patents
Structural concepts for very large (400-meter-diameter) solar concentratorsMikulas Jr et al., 1989
View HTML- Document ID
- 8684516845664579849
- Author
- Mikulas Jr M
- Hedgepeth J
- Carpinteria C
- Publication year
- Publication venue
- Second Beamed Space-Power Workshop, Russell J. De Young, ed., NASA CP-3037
External Links
Snippet
Since the beginning of the space age in the late 1950's, there has been considerable interest in placing large structures in orbit. Most of the applications for these large structures are associated with the reflection of electromagnetic waves. Typical applications include …
- 210000004279 Orbit 0 abstract description 6
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
- B64G1/222—Appendage deployment mechanisms
-
- H—ELECTRICITY
- H01—BASIC ELECTRIC ELEMENTS
- H01Q—AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction, or polarisation of waves radiated from an aerial, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/16—Curved in two dimensions, e.g. paraboloidal
- H01Q15/161—Collapsible reflectors
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
-
- 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
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
-
- 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
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- 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
- B64G1/52—Protection, safety or emergency devices; Survival aids
- B64G1/58—Thermal protection, e.g. heat shields
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Tibert | Deployable tensegrity structures for space applications | |
CA2367979C (en) | Large membrane space structure and method for its deployment and expansion | |
JP2018525265A (en) | Large area structure for compact packaging | |
WO2011006506A1 (en) | Foldable frame supporting electromagnetic radiation collectors | |
Veldman et al. | Inflatable structures in aerospace engineering-an overview | |
Rogers et al. | Technology assessment and development of large deployable antennas | |
Murphey | Historical perspectives on the development of deployable reflectors | |
Swanson et al. | System concept for a moderate cost large deployable reflector (LDR) | |
US5202689A (en) | Lightweight focusing reflector for space | |
RU2627904C2 (en) | Method and device for collecting objects in space with rings and lattice surfaces and method of conclusion of objects in space with flexible, for example, mesh-membrane surfaces | |
Reibaldi et al. | QUASAT program: the ESA reflector | |
Mikulas Jr et al. | Structural concepts for very large (400-meter-diameter) solar concentrators | |
Bernasconi et al. | Inflatable, space-rigidized structures. Overview of applications and their technology impact | |
Kaya et al. | Crawling robots on large web in rocket experiment on Furoshiki deployment | |
Derbes | Case studies in inflatable rigidizable structural concepts for space power | |
Satter et al. | Inflatable structures technology applications and requirements (for space deployable systems) | |
Mikulas Jr et al. | STRUCTURAL CONCEPTS FOR VERY LARGE: _, _-_, c | |
BIRCH | Orbital ring systems and Jacob's Ladders. III | |
Jenkins | Progress in astronautics and aeronautics: gossamer spacecraft: membrane and inflatable structures technology for space applications | |
Schzcerch et al. | Large low-frequency orbiting radio telescope | |
Doggett et al. | In-Space Modular Assembly: An Approach for Reliable, Affordable, Precision Space Apertures | |
Natori et al. | Adaptivity demonstration of inflatable rigidized integrated structures (IRIS) | |
Hedgepeth et al. | Structural concepts for large solar concentrators | |
Hedgepeth | Design concepts for large antenna reflectors | |
Annandale | Thermal and structural analyses of large space antenna reflectors |