Development of a Cold Gas Propulsion System for the ... - SSL - MIT
Development of a Cold Gas Propulsion System for the ... - SSL - MIT Development of a Cold Gas Propulsion System for the ... - SSL - MIT
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26.12.2012
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The first step in calculating
where
- Page 9 and 10: Table of Contents List of Figures .
- Page 11: 7 Ongoing and Future Work .........
- Page 14 and 15: Figure 6-6. Identification of thrus
- Page 17 and 18: Notation Acronyms and Abbreviations
- Page 19 and 20: N newton Pa pascal psi pounds per s
- Page 21 and 22: 1 Introduction The TALARIS (Terrest
- Page 23 and 24: the idea of hopping was born, and i
- Page 25 and 26: However, as stated before, this doe
- Page 27 and 28: Figure 2-3. Diagram of ACAT lander
- Page 29 and 30: An alternate approach to resolving
- Page 31 and 32: accurate conditions for testing GNC
- Page 33 and 34: Ballistic hops tend to use less pro
- Page 35 and 36: 2.3.2 Comparison of Cold Gas and Mo
- Page 37 and 38: Handling propellant There are sever
- Page 39 and 40: and if the cold gas system was foun
- Page 41 and 42: 3 TALARIS CGSE Design Framework Aft
- Page 43 and 44: Figure 3-1. Scaling of TALARIS terr
- Page 45 and 46: (3) Providing attitude control Ther
- Page 47 and 48: Figure 3-2 also shows the body coor
- Page 49 and 50: 4 Modeling and Flow Control Compone
- Page 51 and 52: 4.1.2 Rocket Propulsion Equations L
- Page 53 and 54: variables in equation (4-8) deal wi
- Page 55 and 56: equations. Equation (4-10) was then
- Page 57 and 58: that of helium (0.227 MPa = 32.9 ps
- Page 59: thruster solenoid valve, and chambe
- Page 63 and 64: discussed later in section 6.3.4, t
- Page 65 and 66: The flight profile begins with maxi
- Page 67 and 68: hop, any given valve or regulator o
- Page 69 and 70: esponse time was an important perfo
- Page 71 and 72: directly opens and closes the main
- Page 73 and 74: If 1D isentropic flow is assumed, t
- Page 75 and 76: 5 Single-Stream Component Testing A
- Page 77 and 78: the solenoid valve, and a pressure
- Page 79 and 80: As indicated in Figure 5-3, initial
- Page 81 and 82: Figure 5-5. CGSE high side as const
- Page 83 and 84: Figure 5-7 illustrates several aspe
- Page 85 and 86: 6 Full Eight-Thruster Flight System
- Page 87 and 88: Figure 6-2. TALARIS CGSE assembled
- Page 89 and 90: stream tests revealed that changes
- Page 91 and 92: Figure 6-5. Original CGSE control c
- Page 93 and 94: other constraints. This was difficu
- Page 95 and 96: variables (such as number of thrust
- Page 97 and 98: One solution to this problem would
- Page 99 and 100: One of the characterization tests w
- Page 101 and 102: or more thrusters were firing toget
- Page 103 and 104: Table 6-3. Valve timing metrics dur
- Page 105 and 106: Figure 6-11. Redesigned CGSE contro
- Page 107 and 108: The imaginary simplified thruster c
- Page 109 and 110: traverse phase of a hop and involve
The first step in calculating
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