Maas, 2017 - Google Patents
Development of Pyrolytic Graphite Applications in Spacecraft Thermal Control Systems-Airbus DS NL HiPeR Product Suite Development StatusMaas, 2017
View PDF- Document ID
- 14244703745683787546
- Author
- Maas A
- Publication year
External Links
Snippet
With a twenty times higher thermal conductivity per unit mass than aluminum, pyrolytic graphite offers great potential in the application to spacecraft thermal control systems. Over the last years, Airbus DS NL has been developing thermal control applications for this …
- 230000018109 developmental process 0 title abstract description 22
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
- B64G1/52—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
- B64G1/46—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
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Claricoats et al. | Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance | |
| Maas | Development of Pyrolytic Graphite Applications in Spacecraft Thermal Control Systems-Airbus DS NL HiPeR Product Suite Development Status | |
| Okamoto et al. | On-orbit experiment plan of loop heat pipe and the test results of ground test | |
| Fedele et al. | Aerothermodynamics and thermal design for on-ground and in-flight testing of a deployable heat shield capsule | |
| Elhefnawy et al. | Passive thermal control design and analysis of a university-class satellite | |
| Tomboulian | Lightweight, High-temperature radiator for in-space nuclear-electric power and propulsion | |
| Iwata et al. | Thermal and Structural Performance of a Small Satellite with Networked Oscillating Heat Pipes | |
| Iwata et al. | Evaluation of in-orbit thermal performance of X-ray astronomy satellite “Hitomi” | |
| Hyers et al. | Lightweight, High-Temperature Radiator for Space Propulsion | |
| Iwata et al. | Thermal control system of x-ray astronomy satellite ASTRO-H: current development status and prospects | |
| Mitchao et al. | Preliminary thermal design for microsatellites deployed from International Space Station’s Kibo Module | |
| Nagai et al. | On-orbit demonstration of Advanced Thermal Control Devices using JAXA Rapid Innovative payload demonstration SatellitE-2 (RAISE-2) | |
| Goncharov et al. | High thermal conductive carbon fiber radiators with controlled loop heat pipes | |
| Ferrero et al. | The Challenges of the Thermal Design of BepiColombo Mercury Planetary Orbiter | |
| Lecossais et al. | Deployable panel radiator | |
| Thaikattil | Thermal Analysis and Design of the Photovoltaic Investigation on Lunar Surface (PILS) Payload | |
| Benthem et al. | Innovative new High Performance Radiators: Developing heat rejection systems with flexible film technology | |
| Thaikattil et al. | Thermal Analysis of Photovoltaic Investigation on the Lunar Surface (PILS) | |
| Scigliano et al. | Thermal design of heat pipe cooling systems: conceptual design and numerical development | |
| Foster et al. | Strategies for thermal control of a multifunctional power structure solar array | |
| Mastropietro et al. | Design and Preliminary Thermal Performance of the Mars Science Laboratory Rover Heat Exchangers | |
| Hussain | Thermal Control Design and Analysis of the Optical Telescope of an Earth Observing Satellite | |
| Banisaukas et al. | Carbon fiber composites for spacecraft thermal management opportunities | |
| Zhanli et al. | Thermal control schemes for a micro-satellite with all-active and selectively active solar string designs | |
| Lee et al. | Conceptual thermal design of a network of solar-powered Boardsat-and CubeSat-based landed spacecraft on Mars |