Academic Journal

IN-STEP Inflatable Antenna Description

التفاصيل البيبلوغرافية
العنوان: IN-STEP Inflatable Antenna Description
المؤلفون: Gordon Veal, Robert Freeland, Mr. Robert Freeland
المساهمون: The Pennsylvania State University CiteSeerX Archives
المصدر: http://jpltrs.jpl.nasa.gov/1995/95-1193.pdf.
سنة النشر: 1995
المجموعة: CiteSeerX
الوصف: Large size space deployable antenna structures are needed for a variety of applications. Current resources limitations within the antenna user community have resulted in the need for low cost, light weight and mechanically reliable space structures. An inflatable deployable antenna concept, under development at L'Garde has such great potential for these requirements; it was selected for a NASA sponsored Space Technology Experiment Program (IN-STEP) flight experiment. The objectives of the experiment are to verify low cost and light weight by building a 14 meter-diameter reflector antenna structure and demonstrate deployment reliability and reflector surface precision in a realistic operational environment. The approach will utilize the Space Transportation System (STS) launched recoverable Spartan spacecraft as the experiment carrier. The basic experiment subsystems and their functions include (a) the inflatable structure that consists of: a thin membrane reflector struct.
نوع الوثيقة: text
وصف الملف: application/pdf
اللغة: English
Relation: http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.32.628; http://jpltrs.jpl.nasa.gov/1995/95-1193.pdf
الاتاحة: http://citeseerx.ist.psu.edu/viewdoc/summary?doi=10.1.1.32.628
http://jpltrs.jpl.nasa.gov/1995/95-1193.pdf
Rights: Metadata may be used without restrictions as long as the oai identifier remains attached to it.
رقم الانضمام: edsbas.F080B6A7
قاعدة البيانات: BASE