42 A. Holness et al. Fig. 6.4 Testing results for solar cell wings. (a) Achievable amplitude with full amplitude commanded. (b) Modeled and measured thrust at full commanded amplitude. (c) Achievable amplitude with half amplitude commanded. (d) Modeled and measured thrust at half commanded amplitude Fig. 6.5 Amplitude and thrust of regular wings compared to solar cell wings. (a) Achievable amplitude with full amplitude commanded. (b) Modeled and measured thrust at full commanded amplitude
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