The International Handbook of Space Technology 2014
DOI: 10.1007/978-3-642-41101-4_25
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Mission and System Design

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“…The slope and intercept then correspond to the parameters n and K , respectively, and the resultant curve is shifted to determine the onset time of crystallization. Table presents the fitted values for the three different samples, including the crystallization halftime t 1/2 , which is given by …”
Section: Resultsmentioning
confidence: 99%
“…The slope and intercept then correspond to the parameters n and K , respectively, and the resultant curve is shifted to determine the onset time of crystallization. Table presents the fitted values for the three different samples, including the crystallization halftime t 1/2 , which is given by …”
Section: Resultsmentioning
confidence: 99%
“…The space mission analysis and design activity aims at defining a space system that meets the mission requirements at the minimum over-all cost and risk [26]. The result may include spacecraft's systems and subsystems (e.g., payload, power, structure, attitude, communication, thermal), the mission planning and scheduling (from launch phase to operations, and ultimately spacecraft disposal), the ground segment (e.g., ground stations, control centers) and launch segment (e.g., launch facility, launch vehicle).…”
Section: The Role Of Space Mission Analysis and Designmentioning
confidence: 99%
“…The geometry of the trajectories obtained from MOLTO-IT Step 1 and MOLTO-ITStep 2 are displayed in Fig.5.22a and Fig.5.22b respectively. Detailed results for both mission profiles are presented in Table5 26…”
mentioning
confidence: 99%