Chinese Space Science And Technology.
Abstract
CONTENTS: ABLATIVE THERMAL PROTECTIVE MECHANISM AND NUMERICAL SIMULATION FOR RETURNABLE SATELLITE; ABLATIVE THERMAL PROTECTION STRUCTURE DESIGN OF BALLISTIC RETURN MODULE; THERMAL CONTROL DESIGN OF RETURNABLE SATELLITE; MAIN FACTORS AFFECTING PHOTOGRAPHIC QUALITY OF PRISM SCANNING PANORAMIC CAMERA; ELECTRIC POWER SYSTEM OF RETURNABLE SATELLITES; DEVELOPMENT OF RETURN TECHNOLOGY AND RETURNABLE SPACECRAFT; CHINA'S RETURNABLE SATELLITES; DERIVING RECOVERY MOTION EQUATIONS OF SATELLITE WITH QUATERNION RULE; DIGITAL ATTITUDE CONTROL SYSTEM AND FLIGHT TEST RESULTS OF CHINA'S RETURNABLE SATELLITES. (AN)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 13, 1994
- Accession Number
- ADA289618
Entities
Organizations
- National Air and Space Intelligence Center