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Examinig_ORION_CREW_CAPSULE.pdf | 9 | What are the key features of the Orion crew capsule, and what is the status of its development and testing? | |
Examinig_ORION_CREW_CAPSULE.pdf | 10 | What are the specifications and design considerations for the Space Launch System (SLS), including its initial and future capabilities? | |
Examinig_ORION_CREW_CAPSULE.pdf | 11 | What are the propulsion systems planned for the SLS upper stage, and what is the status of the J-2X engine development? | |
Examinig_ORION_CREW_CAPSULE.pdf | 20 | What is the overall strategy and key milestones for the Exploration Systems Development (ESD) programs, including Orion, SLS, and ground systems? | |
Examinig_ORION_CREW_CAPSULE.pdf | 21 | What are the specific technical advancements and testing activities for the Orion Multi-Purpose Crew Vehicle (MPCV)? | |
Examinig_ORION_CREW_CAPSULE.pdf | 22 | What are the key technical aspects and development status of the Space Launch System (SLS), including its various configurations and engine choices? | |
Examinig_ORION_CREW_CAPSULE.pdf | 23 | What are the plans for the Exploration Ground Systems and how are they integrated with the SLS and Orion programs? | |
Examinig_ORION_CREW_CAPSULE.pdf | 49 | What are the key characteristics of the Space Launch System (SLS) that enable ambitious scientific missions, specifically regarding lift capacity, payload fairing size, and increased energy? | |
Examinig_ORION_CREW_CAPSULE.pdf | 50 | What is the critical factor, beyond technical capabilities, that is essential for the SLS to realize its full scientific potential, and what is the historical precedent for this? | |
Examinig_ORION_CREW_CAPSULE.pdf | 67 | What is the status of the service module design for the Orion spacecraft, and what is the technical risk associated with its development? | |
Examinig_ORION_CREW_CAPSULE.pdf | 68 | Given limited funding, what is the rationale for NASA's decision to pursue an advanced booster competition and development, and what are the implications for the upper stage engine development? | |
Examinig_ORION_CREW_CAPSULE.pdf | 69 | What are the potential destinations that the SLS and Orion can reach beyond LEO, and how does the achievable destination change with different SLS configurations (70 mT, 105 mT, and Block 2/130 mT)? | |
Examinig_ORION_CREW_CAPSULE.pdf | 70 | What critical measures would need to be taken to achieve a crewed SLS/Orion flight capability within this decade, and what are the primary constraints – technical or budgetary? | |
Examinig_ORION_CREW_CAPSULE.pdf | 72 | What are the most significant safety challenges facing Orion, and what are the key elements included in the EFT-1 flight? | |
Examinig_ORION_CREW_CAPSULE.pdf | 73 | What is the impact of reduced funding on the Orion program's ability to demonstrate a fully crew-capable system as part of EM-1 in 2017? | |
Examinig_ORION_CREW_CAPSULE.pdf | 76 | What steps are being taken in the SLS design to promote safety, and what are the key elements of the initial SLS configuration? | |
Examinig_ORION_CREW_CAPSULE.pdf | 77 | What is the significance of the 130 metric ton (mT) LEO performance metric for the SLS, and what alternative metric is suggested for ensuring the vehicle is optimized for Beyond Earth Orbit (BEO) exploration? | |
Examinig_ORION_CREW_CAPSULE.pdf | 78 | What is the schedule for developing a new upper stage powered by the J-2X engine, and to what degree will a new upper stage require modifications and testing of the core stage? | |
Examinig_ORION_CREW_CAPSULE.pdf | 79 | What is the impact of increased funding on the 2017 and 2021 flight schedules for the SLS? | |
Ariane-5-Users-Manual-2000.pdf | 55 | Referring to Figure 2.6.1.a, what are the key steps in a typical spacecraft/SYLDA separation sequence, and what role does the Attitude Control System (SCA) play in each step? | |
Ariane-5-Users-Manual-2000.pdf | 56 | How does the spacecraft separation sequence differ when using SPELTRA compared to SYLDA 5, as illustrated in Figures 2.6.1.a and 2.6.1.b, and what are the implications for the SCA? | |
Ariane-5-Users-Manual-2000.pdf | 57 | Describe the spacecraft separation sequence for a single launch configuration as depicted in Figure 2.6.1.c, and how does the SCA contribute to this sequence? | |
Ariane-5-Users-Manual-2000.pdf | 65 | Based on Figure 3.2.2.a, describe the ventilation system within the payload volume and its purpose. | |
Ariane-5-Users-Manual-2000.pdf | 71 | What is the nature of the 'Spurious Radiation' depicted in Figure 3.5.a, and what are the potential sources? | |
Ariane-5-Users-Manual-2000.pdf | 73 | What are the reference axes for the Ariane 5 launch vehicle, as shown in Figure 4.1.a, and what is their significance? | |
Ariane-5-Users-Manual-2000.pdf | 75 | Describe the SPELTRA external carrying structures as shown in Figure 4.3.1.a, and what is their function? | |
Ariane-5-Users-Manual-2000.pdf | 76 | Describe the SYLDA 5 internal carrying structures as shown in Figure 4.3.1.b, and what is their function? | |
Ariane-5-Users-Manual-2000.pdf | 77 | What does Figure 4.3.1.c illustrate regarding the ACY 5400 and its application? | |
Ariane-5-Users-Manual-2000.pdf | 79 | Describe the single launch bolted interface 2624 as shown in Figure 4.3.5.1.a, and what are its key features? | |
Ariane-5-Users-Manual-2000.pdf | 80 | Describe the dual launch bolted interface 2624 as shown in Figure 4.3.5.1.b, and how does it differ from the single launch interface? | |
Ariane-5-Users-Manual-2000.pdf | 81 | Describe the single launch bolted interface 3936 as shown in Figure 4.3.5.2.a, and how does it differ from the 2624 interface? | |
Ariane-5-Users-Manual-2000.pdf | 82 | What is the purpose of the geometric characteristic symbols and surface roughness symbols, as described in Figure 4.3.5.3, and how are they used? | |
Ariane-5-Users-Manual-2000.pdf | 102 | What are the geographic coordinates of the Guiana Space Centre (CSG), as indicated in Figure 5.4.a, and why is this location significant for launches? | |
Ariane-5-Users-Manual-2000.pdf | 106 | Describe the typical operations flow diagram as shown in Figure 5.4.e, and what are the key stages involved? | |
Ariane-5-Users-Manual-2000.pdf | 113 | Describe the typical single launch encapsulation sequence as shown in Figure 5.4.3.1.b, and what are the key steps? | |
Ariane-5-Users-Manual-2000.pdf | 114 | Describe the typical dual launch encapsulation sequence with SPELTRA as shown in Figure 5.4.3.1.c, and what are the key steps? | |
Ariane-5-Users-Manual-2000.pdf | 115 | Describe the typical dual launch encapsulation sequence with SYLDA 5 as shown in Figure 5.4.3.1.d, and what are the key steps? | |
Ariane-5-Users-Manual-2000.pdf | 127 | Describe the typical control center configuration for an Ariane launch as shown in Figure 5.5.b, and what are the key elements? | |
Ariane-5-Users-Manual-2000.pdf | 132 | What is the purpose of the time schedule of documentation and reviews as shown in Figure 6.1.a? | |
Ariane-5-Users-Manual-2000.pdf | 184 | What are the key structural and mechanical features of the Ariane 5 937VB5 adaptor, including materials, dimensions, separation mechanisms, and force specifications? | |
Ariane-5-Users-Manual-2000.pdf | 193 | Describe the key structural and mechanical characteristics of the Ariane 5 1194V5 adaptor, including materials, dimensions, separation mechanisms, and force specifications. | |
Ariane-5-Users-Manual-2000.pdf | 203 | What are the key design features of the 1194H clampband, as described on this page, and what are the implications of these features? | |
Ariane-5-Users-Manual-2000.pdf | 212 | What is the significance of the 'Limit loads of adaptor 1663SP5 at separation plane' shown in Figure A9-1, and what type of loads are likely to be considered? | |
Ariane-5-Users-Manual-2000.pdf | 214 | Based on Figure A9-3 and A9-4, describe the mechanical interface principle of the 1663SP5 adaptor and the key design elements of the interface. | |
Ariane-5-Users-Manual-2000.pdf | 220 | What is the significance of the 'Limits loads of adaptor 1666V5 at separation plane' shown in Figure A10-1, and what type of loads are likely to be considered? | |
Ariane-5-Users-Manual-2000.pdf | 223 | Based on Figure A10-4, describe the mechanical interface details of the 1666V5 adaptor. | |
Ariane-5-Users-Manual-2000.pdf | 228 | What is the significance of the 'Limit loads of adaptor 2624' shown in Figure A11-1? | |
Ariane-5-Users-Manual-2000.pdf | 236 | Describe the key components and functionality of the Ariane multipurpose boom dispenser, as depicted in Figure 12.1. | |
Ariane-5-Users-Manual-2000.pdf | 237 | What are the key features of the multipurpose platform dispenser, as shown in Figure 12.2? |
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