Title :
Low-cost, risk-reduction testing of class D spacecraft photovoltaic systems
Author :
Forgione, Joshua B. ; Kojima, Gilbert ; Hanel, Robert ; Mallinson, Mark
Author_Institution :
NASA Ames Res. Center, Mountain View, CA, USA
Abstract :
The end-to-end verification of a spacecraft photovoltaic power generation system requires light! A low-cost, portable, and end-to-end photovoltaic-system test appropriate for NASA´s new generation of Class D missions is presented. High risk, low-cost, and quick-turn satellites rarely have the resources to execute the traditional approaches from higher-class (A-C) missions. The Class D approach, as demonstrated on the Lunar Atmospheric and Dust Environment Explorer (LADEE), utilizes a portable, metal-halide, theatre lamp for an end-to-end photovoltaic system test. While not as precise and comprehensive as the traditional Large Area Pulsed Solar Simulator (LAPSS) test, the LADEE method leverages minimal resources into an ongoing assessment program that can be applied through numerous stages of the mission. The project takes a true Class D approach in assessing the technical value of a costly, high-fidelity performance test versus a simpler approach with less programmatic risk. The resources required are a fraction of that for a LAPSS test, and is easy to repeat due to its portability. Further, the test equipment can be handed down to future projects without building an on-site facility. At the vanguard of Class D missions, the LADEE team frequently wrestled with and challenged the status quo. The philosophy of risk avoidance at all cost, typical to Class A-C missions, simply could not be executed. This innovative and simple testing solution is contextualized to NASA Class D programs and a specific risk encountered during development of the LADEE Electrical Power System (EPS). Selection of the appropriate lamp and safety concerns are discussed, with examples of test results. Combined with the vendor´s panel-level data and periodic inspection, the method ensures system integrity from Integration and Test (I&T) through launch. Following launch, mission operations tools are utilized to assess system performance based on a scant amount of available data.
Keywords :
aerospace safety; aerospace testing; aircraft power systems; inspection; lamps; photovoltaic power systems; portable instruments; space vehicles; test equipment; A-C mission; EPS; I&T; LADEE; LAPSS testing; Lunar Atmospheric and Dust Environment Explorer; NASA; class D spacecraft photovoltaic power generation system; electrical power system; higher-class mission; integration and test; large area pulsed solar simulator test; periodic inspection; portable metal-halide theatre lamp; risk avoidance philosophy; risk-reduction testing; satellite; test equipment; vendor panel- level data; Arrays; NASA; Observatories; Photovoltaic systems; Satellites; Space vehicles; Testing;
Conference_Titel :
Aerospace Conference, 2014 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5582-4
DOI :
10.1109/AERO.2014.6836459