[go: up one dir, main page]

Gilmore, 2002 - Google Patents

6 Radiators

Gilmore, 2002

View PDF
Document ID
9043089894417820989
Author
Gilmore D
Publication year

External Links

Snippet

Spacecraft waste heat is ultimately rejected to space by radiator surfaces. Radiators occur in several different forms, such as spacecraft structural panels, fiat-plate radiators mounted to the side of the spacecraft, and panels deployed after the spacecraft is on orbit. Whatever the …
Continue reading at matthewwturner.com (PDF) (other versions)

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
    • B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/50—Arrangements or adaptations of devices for control of environment or living conditions for temperature control
    • B64G1/503—Radiator panels
    • 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
    • B64G1/22—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F24—HEATING; RANGES; VENTILATING
    • F24J—PRODUCING OR USE OF HEAT NOT OTHERWISE PROVIDED FOR
    • F24J2/00—Use of solar heat, e.g. solar heat collectors
    • F24J2/04—Solar heat collectors having working fluid conveyed through collector
    • F24J2/06—Solar heat collectors having working fluid conveyed through collector having concentrating elements
    • F24J2/10—Solar heat collectors having working fluid conveyed through collector having concentrating elements having reflectors as concentrating elements
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GASES [GHG] EMISSION, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/40—Solar thermal energy
    • 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
    • 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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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

Similar Documents

Publication Publication Date Title
US9889951B1 (en) Spacecraft east-west radiator assembly
JPH1191699A (en) High power spacecraft using whole surface thereof
US20170328654A1 (en) Variable Heat Rejection Device
Gilmore 6 Radiators
Ponnappan et al. High-power thermal management issues in space-based systems
KR20250026294A (en) Satellite thermal control
Bhandari et al. Mars Science Laboratory thermal control architecture
Lashley et al. Deployable radiators-A multi-discipline approach
Choi Thermal design to meet stringent temperature gradient/stability requirements of SWIFT BAT detectors
Lécossais et al. Deployable panel radiator
Williams Robust satellite thermal control using forced air convection thermal switches for operationally responsive space missions
Oleson et al. A kuiper belt object orbiter enabled by 10 kW kilopower electric propulsion
CHALMERS et al. Application of capillary pumped loop heat transport systems to largespacecraft
Miao et al. Typical Thermal Control Technologies for Spacecraft
Herrin et al. Preliminary design of the space station internal thermal control system
Choi Thermal assessment of swift instrument module thermal control system and mini heater controllers after 5+ Years in Flight
Kirkpatrick et al. Advanced thermal control flight experiment
SULLIVAN Selection of space radiator systems to meet advanced mission requirements
Steinfeld et al. Passive freeze protection for the international space station photovoltaic radiators
Ku et al. Thermal performance of capillary pumped loops onboard Terra Spacecraft
Miao et al. Typical Thermal Control Design Cases of Spacecraft
Walimbe et al. Evolutionary insights into the state-of-the-art passive thermal control systems for thermodynamic stability of smallsats
Choi Thermal Assessment of Swift Instrument Module Thermal Control System during First 2.5 Years in Flight
Roukis et al. COMET Service Module Thermal Control System Design Using a Capillary Pumped Loop
Choi Utilization of Waste Heat to Warm Optical Telescopes or Lasers in Space by Using Loop Heat Pipes