Wrinkle Reduction Design Method of Triangular Solar Sail
نویسندگان
چکیده
منابع مشابه
AIAA 2002-1703 Scalable Solar Sail Subsystem Design Considerations
Under recent contract to JPL for the New Millennium Space Technology 7 Program (ST7) AEC-Able Engineering (ABLE) developed a Scalable Solar Sail Subsystem (S). The S is a minimal mass propulsion subsystem that can be mounted to a general heritage spacecraft to provide continuous low level thrust. The design baseline is a 3-axis-stabilized 4-quadrant square sail with attitude controlled through ...
متن کاملElectric Solar Wind Sail Mass Budget Model
The electric solar wind sail (E-sail) is a new type of propellantless propulsion system for Solar System transportation, which uses the natural solar wind for producing spacecraft propulsion. This paper discusses a mass breakdown and a performance model for 5 an E-sail spacecraft that hosts a scientific payload of prescribed mass. In particular, the model is able to estimate the total spacecraf...
متن کاملAccessing the Solar System With a Small Solar Sail
Solar sailing is a proposed means of space propulsion in which a reflective surface collects momentum from solar photons to accelerate a vehicle. The current trend within the solar sailing community is to increase sail size as solar sailing technologies advance, allowing for larger payloads and higher accelerations. However, with the miniaturization of modern payloads, sail sizes can be dramati...
متن کاملSolar Sail Science Mission Applications and Advancement
Solar sailing has long been envisaged as an enabling or disruptive technology. The promise of openended missions allows consideration of radically new trajectories and the delivery of spacecraft to previously unreachable or unsustainable observation outposts. A mission catalogue is presented of an extensive range of potential solar sail applications, allowing identification of the key features ...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Journal of the Korean Society for Aeronautical & Space Sciences
سال: 2013
ISSN: 1225-1348
DOI: 10.5139/jksas.2013.41.12.940