| タイトル | Iodine Propulsion Advantages for Low Cost Mission Applications and the Iodine Satellite (ISAT) Technology Demonstration |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150021456 |
| 著者（英） | Schumacher, Daniel M.; Dankanich, John W. |
| 発行日 | 2015-10-12 |
| 言語 | eng |
| 内容記述 | The NASA Marshall Space Flight Center Science and Technology Office is continuously exploring technology options to increase performance or reduce cost and risk to future NASA missions including science and exploration. Electric propulsion is a prevalent technology known to reduce mission costs by reduction in launch costs and spacecraft mass through increased post launch propulsion performance. The exploration of alternative propellants for electric propulsion continues to be of interest to the community. Iodine testing has demonstrated comparable performance to xenon. However, iodine has a higher storage density resulting in higher V capability for volume constrained systems. Iodine's unique properties also allow for unpressurized storage yet sublimation with minimal power requirements to produce required gas flow rates. These characteristics make iodine an ideal propellant for secondary spacecraft. A range of mission have been evaluated with a focus on low-cost applications. Results highlight the potential for significant cost reduction over state of the art. Based on the potential, NASA has been developing the iodine Satellite for a near-term iodine Hall propulsion technology demonstration. Mission applications and progress of the iodine Satellite project are presented. |
| NASA分類 | Spacecraft Propulsion and Power; Propellants and Fuels |
| レポートNO | IAC-15-D2.5.7x31069
M15-4895 |
| 権利 | No Copyright |
