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Table 1. Mission Types vs. Mission Facets

in Autonomous Mobile Robots and Distributed Exploratory Missions
by Dean F. Hougen, Michael D. Erickson, Paul E. Rybski, Sascha A. Stoeter, Maria Gini, Nikolaos Papanikolopoulos 2000
"... In PAGE 5: ... 2.1 are summarized in Table1 . In the table, `Y apos; indicates the mission has this facet, `N apos; that it does not, and `? apos; that it may vary and is, therefore, discussed below.... ..."
Cited by 3

Table 1. Mission Modes

in CubeSat Design for LEO-Based Earth Science Missions
by Stephen Waydo Daniel
"... In PAGE 2: ... Both of these procedures will be discussed in more detail in section 5, Attitude Control, below. Mission Modes Table1 defines the modes of operation of the CubeSat system. Table 1.... ..."

Table 2. Mission characteristics.

in Determination Of The Gravity Field From Satellite Gradiometry - A Simulation Study
by Michael Belikov, Martin van Gelderen, Radboud Koop 1994
Cited by 2

Table 2. The mission parameters

in The Use of Degree Variances in Satellite Gradiometry
by Martin van Gelderen, Radboud Koop 1997
Cited by 1

Table 2. Mission metrics

in A Three-tiered Evaluation Approach for Interactive Spoken Dialogue Systems
by Kathleen Stibler, James Denny
Cited by 1

TABLE 2 Duck Missions

in Chemical Plume Mapping with an Autonomous Underwater Vehicle
by Barbara Fletcher

Table 4 Missions

in Applications for mini VTOL UAV for law enforcement
by Douglas Murphy, James Cycon

Table 1. ISC Branches and their Missions

in unknown title
by unknown authors 1999
"... In PAGE 8: .................. 5-11 Tables Table1 . ISC Branches and their Missions .... ..."

Table 1: CSA Mission Specifications

in Development of a Multi-Mission Sizing Methodology Applied to the Common Support Aircraft
by Dimitrin Mavris And
"... In PAGE 4: ...17 Table 4: Calibration of FLOPS Output to S-3A Data MISSION SPACE EXPLORATION The creation of the mission space begins with parameterization of the requirements into mission space variables. Referring again to Table1 , it is seen that each support mission can be thought of in terms of a generic model with nine variable segments. These are (1) warm up, taxi, and takeoff, (2) climb, (3) cruise, (4) loiter, (5) weapons release, (6) return cruise, (7) descent, (8) loiter, and (9) landing.... ..."

Table 3 Mission Time [days]

in Rover design for polar astrobiological exploration
by Liam Pedersen, David Wettergreen, Dimi Apostolopoulos, Chris Mckay, Matthew Digoia 2005
"... In PAGE 7: ...the former two by the net energy generated in charge mode. Table3 summarizes the mission time breakdown for Nomad as currently configured, and with proposed modifications for the mission. These times assume an average of 17W and 343W wind and solar power respectively.... ..."
Cited by 1
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