CFRP integral technology of satellite payload attach fitting
Abstract
The structures of payload attach fitting (PAF) are presented with the introduction of PAF-I used for N-II rocket third stage, PAF-IV used for H-I rocket second stage, and PAF-VI used for H-II rocket second stage. The CFRP integral processing technology of the PAT is addressed.
- Publication:
-
Japan Society of Composite Materials Journal
- Pub Date:
- 1992
- Bibcode:
- 1992JSCMJ..18...39K
- Keywords:
-
- Carbon Fiber Reinforced Plastics;
- Japanese Spacecraft;
- Multistage Rocket Vehicles;
- Payload Integration;
- Satellite Configurations;
- Aluminum Alloys;
- Temperature Gradients;
- Launch Vehicles and Space Vehicles