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).


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