labels.csv

Text
\ref{chap:cfd-appendix}
\ref{}
\ref{}
\ref{cfd-stremlines}
\ref{chap:nasa-payload}
\ref{sec:nasa-payload:mech-design}
\ref{subsec:nasa-payload:mech-design:changes}
\ref{subsubsec:nasa-payload:mech-design:Antenna-Design}
\ref{subsubsec:nasa-payload:design-overview:antenna-deployment}
\ref{fig:payload:ant-deployment-system-constructed}
\ref{subsubsec:nasa-payload:design-overview:stemcraft-design}
\ref{fig:payload:stemcraft-internals-constructed}
\ref{subsec:nasa-payload:elec-design:Construction}
\ref{tab:payload:construction:rotating-mount}
\ref{tab:payload:construction:antenna-assembly}
\ref{tab:payload:construction:stemcraft-integration}
\ref{fig:payload:bulk-assembly-drawing}
\ref{fig:payload:ant-assembly-drawing}
\ref{sec:nasa-payload:electronics-design}
\ref{subsec:nasa-payload:electronics-design:changes}
\ref{subsec:nasa-payload:electronics-design:Unique-Features}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:schematic}
\ref{fig:payload:block_diagram_1}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:data-collection}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:Safety}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:payload-to-transceiver}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:team-to-payload}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:Code-Logic}
\ref{fig:payload:electricaldesign:esp32codelogic}
\ref{subsubsec:nasa-payload:electronics-design:Unique-Features:PCB}
\ref{fig:payload:pcb_V1}
\ref{subsec:nasa-payload:elec-design::schematic}
\ref{fig:payload:schematic_V1}
\ref{subsec:nasa-payload:elec-design:Construction}
\ref{fig:payload:soldering_1}
\ref{fig:paylaod:micro_soldering_1}
\ref{fig:payload:not_holding_antenna_1}
\ref{fig:paylaod:holding_antenna_1}
\ref{tab:nasa-payload:construction}
\ref{subsec:nasa-payload:flight_reliability_confidence}
\ref{subsec:nasa-payload:elec-design:stemcraft-design:stemcraft-retention}
\ref{fig:payload:pcb_dimensions_1}
\ref{sec:ads-payload:planned-payload-demonstration-flight}
\ref{chap:ads-payload}
\ref{sec:ads-payload:mech-design-testing}
\ref{subsec:ads-payload:mech:summary-of-changes-since-cdr}
\ref{subsec:ads-payload:overview}
\ref{fig:ads-structural-assembly}
\ref{subsec:ads-payload:flight-reliability-confidence}
\ref{fig:ads-drag-force-vs-reynolds-number}
\ref{fig:ads-cp-distance-vs-reynolds-number}
\ref{fig:ads-cd-vs-reynolds-number}
\ref{subsec:ads-payload:construction}
\ref{subsubsec:ads-payload:construction:flaps-links-pinion}
\ref{tab:ads:FLPPconstruction_steps}
\ref{fig:FLPP_step1}
\ref{fig:FLPP_Step2}
\ref{fig:FLPP_step3}
\ref{fig:FLPP_steps}
\ref{subsubsec:ads-payload:construction}
\ref{tab:construction-baseplatesteps}
\ref{fig:construction-baseplate_waterjet}
\ref{fig:construction-baseplate_step2}
\ref{fig:construction-baseplate_step3}
\ref{fig:construction-baseplate_steps}
\ref{subsubsec:ads-payload:construction}
\ref{tab:ads:flapband_construction_steps}
\ref{fig:construction-flapband_step1}
\ref{fig:construction-flapband_step2}
\ref{fig:construction-flapband_step3}
\ref{fig:construction-flapband_step4}
\ref{fig:construction-flapbandsteps}
\ref{subsubsec:ads-payload:construction:integration}
\ref{tab:ads:integration-steps}
\ref{fig:ads:pcb_with_kinematics}
\ref{fig:ads:on_threaded_rods}
\ref{fig:ads:full_flapband_integration}
\ref{subsec:ads-payload:elec:summary-of-changes-since-cdr}
\ref{fig:ads:v1_top}
\ref{fig:ads:v2_top}
\ref{fig:ads:pcb_fully_integrated}
\ref{subsec:ads-payload:schematic}
\ref{fig:ads:schematic}
\ref{subsubsec:ads-payload:overview:electrical-elements}
\ref{subsubsec:ads-payload:construction}
\ref{tab:ads-payload:construction}
\ref{fig:ads:flowchat}
\ref{sec:ads-payload:schematics-of-as-built-payload}
\ref{fig:ads-kinematic-subassembly-as-built}
\ref{fig:ads-full-assembly-as-built}
\ref{fig:ads:dimensional_drawing_1}
\ref{sec:ads-payload:planned-payload-demonstration-flight}
\ref{sec:ads-payload:conops}
\ref{fig:ads:ads-conops}
\ref{sec:ads-payload:design-overvoew}
\ref{sec:ads-payload:design-overview:drawing-packet}
\ref{sec:ads-payload:design-overview:drawing-packet:assembly-level-drawings}
\ref{fig:ads:ads-full-assembly}
\ref{fig:ads:ads-kinematic-subassy}
\ref{fig:ads:ads-mounting-subassy}
\ref{fig:ads:ads-fwd-flap-subassy}
\ref{fig:ads:ads-pinion-plate-subassy}
\ref{fig:ads:ads-linkage-subassy}
\ref{fig:ads:ads-electronics-subassy}
\ref{fig:ads:ads-servo-subassy}
\ref{fig:ads:ads-fwd-bulkhead-subassy}
\ref{fig:ads:ads-aft-bulkhead-subassy}
\ref{sec:ads-payload:design-overview:drawing-packet:part-level-drawings}
\ref{fig:ads:ads-coupler}
\ref{fig:ads:ads-flap-band}
\ref{fig:ads:base-plate}
\ref{fig:ads:pinion-plate}
\ref{fig:ads:flap}
\ref{fig:ads:linkage}
\ref{fig:ads:electronics-tray}
\ref{fig:ads:alignment-feature}
\ref{fig:ads:aft-bulkhead}
\ref{fig:ads:forward-bulkhead}
\ref{subsec:ads-interface-lv}
\ref{fig:ads:interfaces}
\ref{fig:ads:load-path}
\ref{sec:ads-payload:leading-design}
\ref{subsec:ads-payload:leading-design:sparc}
\ref{subsubsec:ads-payload:leading-design:sparc:code-flow}
\ref{fig:ads:sparc-code-flowchart}
\ref{subsubsec:ads-payload:leading-design:sparc:hardware-integration}
\ref{subsubsec:ads-payload:leading-design:sparc:validation}
\ref{ads-testing-code}
\ref{6dof-validation}
\ref{ads-block-diagram}
\ref{ads-calibration-procedure}
\ref{ads-schematic}
\ref{chap:ads-cad-files}
\ref{fig:ads-full-assembly-drawing}
\ref{fig:ads-mounting-subassembly-drawing}
\ref{fig:ads-kinematic-subassembly-drawing}
\ref{fig:ads-electronics-subassembly-drawing}
\ref{fig:ads-pinion-plate-subassembly-drawing}
\ref{fig:ads-linkage-subassembly-drawing}
\ref{fig:ads-flap-subassembly-drawing}
\ref{fig:ads-servo-subassembly-drawing}
\ref{fig:ads-fwd-bulkhead-subassembly-drawing}
\ref{fig:ads-aft-bulkhead-subassembly-drawing}
\ref{fig:ads-coupler-drawing}
\ref{fig:ads-flap-band-drawing}
\ref{fig:ads-fwd-bulkhead-drawing}
\ref{fig:ads-aft-bulkhead-drawing}
\ref{fig:ads-aft-bulkhead-drawing}
\ref{fig:ads-base-plate-drawing}
\ref{fig:ads-electronics-tray-drawing}
\ref{fig:ads-pinion-plate-drawing}
\ref{fig:ads-linkage-drawing}
\ref{fig:ads-flap-drawing}
\ref{fig:ads-alignment-feature-drawing}
\ref{fig:ads-switch-holder-drawing}
\ref{chap:changes-since-pdr}
\ref{chap:wind-tunnel-test-plan-appendix}
\ref{fig:wind-tunnel-appendix:wind-tunnel-visualizer}
\ref{fig:gooners}
\ref{fig:gooners}
\ref{fig:gooners}
\ref{fig:gooners}
\ref{fig:gooners}
\ref{tab:wind-tunnel-appendix:procedurenomenclature}
\ref{tab:nomenclature}
\ref{tab:wind-tunnel-appendix:abbtestmatrix}
\ref{tab:wind-tunnel-appendix:time}
\ref{tab:wind-tunnel-appendix:timeest}
\ref{tab:outputs}
\ref{tab:sample-data-points-with-expected-results}
\ref{Manual actuation distance}
\ref{tab:manual_ads_testing_estimates}
\ref{chap:safety}
\ref{sec:launch-procedures-and-checklists}
\ref{tab:launch-procedures-toc}
\ref{sec:safety:personnel-hazard-analysis}
\ref{sec:safety:fmea}
\ref{sec:safety:environmental-risks}
\ref{chap:analysis-appendix}
\ref{appendix:analysis:lv}
\ref{appendix:analysis:lv:parachute-shock-force}
\ref{tab:known-values-for-parachute-shock-force-analysis}
\ref{eqn:opening-time}
\ref{tab:calculate-parachute-opening-time}
\ref{eqn:ballistic-parameter}
\ref{tab:calculate-ballistic-parameter}
\ref{fig:opening-force-reduction-factor-plot-from-knacke}
\ref{eqn:parachute-opening-shock-force}
\ref{tab:calculate-parachute-opening-shock-force}
\ref{appendix:analysis:lv:energetics-sizing}
\ref{eqn:bolt-shear-failure}
\ref{eqn:bolt-shear-failure2}
\ref{appendix:analysis:lv:energetics-sizing:shear-pins}
\ref{tab:parameters}
\ref{appendix:analysis:lv:energetics-sizing:charge_sizing}
\ref{appendix:analysis:lv:fin-normal-force}
\ref{eqn:lift}
\ref{eqn:coefficient-of-lift}
\ref{tab:appendix:analysis:lv:fin-normal-force-calculations}
\ref{appendix:analysis:lv:fin-flutter}
\ref{eq:fin flutter}
\ref{fig:analysis:cdr-fin-drawing}
\ref{eq:speed of sound}
\ref{eq:temperature at altitude}
\ref{eq:aspect ratio}
\ref{tab:appendix:analysis:fin-fin-flutter-and-divergence-calculations}
\ref{tab:appendix:analysis:flutter-velocity-margin}
\ref{appendix:analysis:lv:thrust-plate-fea-analysis}
\ref{fig:analysis:thrust-plate-fea}
\ref{appendix:analysis:lv:ballast-washers-fea-analysis}
\ref{fig:analysis:3.74lb-Stress-FEA}
\ref{fig:analysis:1.10lb-Stress-FEA}
\ref{fig:analysis:0.66lb-Stress-FEA}
\ref{fig:analysis:0.33lb-Stress-FEA}
\ref{fig:analysis:0.11lb-Stress-FEA}
\ref{appendix:analysis:lv:recovery-loads}
\ref{eqn:main-recovery-loads}
\ref{tab:appendix:analysis:recovery-loads-hand-calculations}
\ref{fig:analysis:descent-dynamics}
\ref{eq:appendix:analysis:lv:pressure}
\ref{tab:appendix:analysis:lv:recovery-metal-stress}
\ref{appendix:analysis:lv:energetics-sizing}
\ref{eqn:bolt-shear-failure}
\ref{eqn:bolt-shear-failure2}
\ref{appendix:analysis:lv:energetics-sizing:shear-pins}
\ref{tab:parameters}
\ref{appendix:analysis:lv:energetics-sizing:charge_sizing}
\ref{sec:analysis-appendix:stemcraft-payload}
\ref{subsec:analysis-appendix:stemcraft-payload:antenna-bending-calculations}
\ref{tab:appendix:analysis:copper-fiberglass-bending}
\ref{tab:appendix:analysis:load-deflection}
\ref{tab:appendix:analysis:bending-stress}
\ref{appendix:analysis:nasa-payload:transmission-range}
\ref{fig:analysis:radio-distance-diagram}
\ref{sec:analysis-appendix:ads-payload}
\ref{appendix:analysis:ads-payload:mounting-hardware-sizing}
\ref{tab:appendix:analysis:ads-payload:forward-u-bolt}
\ref{tab:appendix:analysis:ads-payload:threaded-rods}
\ref{tab:appendix:analysis:ads-payload:aft-motor-stud}
\ref{appendix:analysis:ads-payload:flap-loading}
\ref{fig:analysis:drag-induced-bending-diagram}
\ref{fig:analysis:static-pitch-moment-rating}
\ref{tab:appendix:analysis:drag-induced-bending-moment}
\ref{appendix:analysis:ads-payload:1dof-model}
\ref{fig:analysis:1dof}
\ref{chap:lv}
\ref{sec:lv:vehicle-criteria}
\ref{subsec:lv:vehicle-criteria:changes}
\ref{subsec:lv:vehicle-criteria:design-and-construction-of-launch-vehicle}
\ref{fig:lv:leading-design-OR}
\ref{subsubsec:lv:vehicle-criteria:layout-and-separation points}
\ref{subsubsec:lv:vehicle-criteria:primary-structure}
\ref{fig:lv:nose-cone-fiberglass-drawing}
\ref{fig:lv:nose-cone-tip-drawing}
\ref{fig:lv:structure:forward-airframe-drawing}
\ref{fig:lv:aft-airframe-drawing}
\ref{fig:lv:booster-airframe-drawing}
\ref{subsubsec:lv:vehicle-criteria:onboard-video}
\ref{fig:lv:pcb_mount_drawing}
\ref{fig:lv:shroud_drawing}
\ref{fig:lv:camera_components}
\ref{fig:lv:mounted_housing}
\ref{fig:lv:pcb_drawing}
\ref{fig:lv:video_drawing}
\ref{fig:lv:pcb_video_drawing}
\ref{fig:lv:nose-cone-coupler}
\ref{fig:lv:payload-switchband}
\ref{fig:lv:nose-cone-components}
\ref{tab:lv:onboard-video-construction}
\ref{fig:lv:mounted_cam}
\ref{fig:lv:finished_cam_mount}
\ref{fig:lv:installed_housing}
\ref{fig:lv:cam_mount_comparison}
\ref{subsubsec:lv:vehicle-criteria:fin-shape-and-material}
\ref{fig:lv:fin_clamp}
\ref{tab:FinWaterjet}
\ref{fig:lv:fin_waterjet}
\ref{subsubsec:lv:vehicle-criteria:fin-clamps}
\ref{fig:lv:clamp}
\ref{fig:lv:clamp_drawing}
\ref{fig:lv:clamp_tensile_test}
\ref{fig:lv:slip_fit_test}
\ref{fig:lv:rectilinear_plot}
\ref{fig:lv:triangular_plot}
\ref{fig:lv:gyroid_plot}
\ref{fig:lv:stress_strain_plots}
\ref{tab:ClampConstruction}
\ref{fig:lv:fin-clamp-subassembly-drawing}
\ref{fig:lv:fin-system-assembly}
\ref{subsubsec:lv:vehicle-criteria:motor-mounting}
\ref{fig:thrust_and_centering}
\ref{tab:CRTPConstruction}
\ref{fig:centering_ring_drawing}
\ref{fig:thrust_plate_drawing}
\ref{subsubsec:lv:vehicle-criteria:ballast}
\ref{fig:lv:Ballast_In_Context}
\ref{fig:lv:Ballast_1.10lb_Washer}
\ref{fig:lv:Ballast_0.66lb_Washer}
\ref{fig:lv:Ballast_0.33lb_Washer}
\ref{fig:lv:Ballast_0.11lb_Washer}
\ref{fig:lv:Ballast_Washers}
\ref{tab:Ballast_Construction}
\ref{subsubsec:lv:vehicle-criteria:mass-properties}
\ref{tab:mass-prop}
\ref{sec:lv:recovery-subsystem}
\ref{subsec:lv:recovery-subsystem:as-built design}
\ref{fig:DSDD Recovery System}
\ref{subsubsec:lv:recovery-subsystem:as-built design:parachutes}
\ref{subsubsec:lv:recovery-subsystem:as-built design:shock-cord}
\ref{fig:Kevlar Shock Cord}
\ref{subsubsec:lv:recovery-subsystem:as-built design:attachment-hardware}
\ref{subsubsec:lv:recovery-subsystem:as-built design:energetics-sizing}
\ref{subsubsec:lv:recovery-subsystem:as-built design:electrical-components-and-redundancy}
\ref{fig:lv:mission_preformance:wiring}
\ref{subsubsec:lv:recovery-subsystem:as-built design:avionics-stack}
\ref{fig:avionics-assembly}
\ref{fig:avionics-wiring}
\ref{tab:Avionics Stack Construction}
\ref{fig:avionics-bulkheads}
\ref{fig:bulkheadone}
\ref{fig: avionics-sled-cad}
\ref{fig:avionics-stack-wired}
\ref{fig:full-avionics-stack-constructed}
\ref{fig:avionics-switchband}
\ref{fig:avionics-coupling-tube}
\ref{fig:lv:avionics-switchband-and-coupling-tube}
\ref{fig:avionics-sled-subassembly}
\ref{fig:constructed-avionics-subassembly}
\ref{fig:avionics-sled-body}
\ref{fig:avionics-bulkhead-subassembly}
\ref{fig:bulkheadone}
\ref{fig:avionics-bulkhead-subassembly}
\ref{fig:avionics-bulkhead-body}
\ref{fig:charge-well}
\ref{sec:lv:mission-performance-predictions}
\ref{subsec:lv:mission-performance-predictions:methods}
\ref{subsec:lv:mission-performance-predictions:flight-profile-simulations}
\ref{subsubsec:lv:mission-performance-predictions:flight-profile-simulations:simulation-conditions}
\ref{tab:lv:mission_preformance:or_sim_conditions}
\ref{tab:lv:mission_preformance:ras_sim_conditions}
\ref{subsubsec:lv:mission-performance-predictions:flight-profile-simulations:openrocket-simulation-results}
\ref{tab:lv:mpp:or_simulation_results}
\ref{fig:lv:mission_preformance:or_height}
\ref{fig:lv:mission_preformance:or_velocity}
\ref{fig:lv:mission_preformance:or_accel}
\ref{tab:lv:mpp:ras_results}
\ref{tab:lv:mpp:ras_results}
\ref{fig:lv:mission_preformance:ras_height}
\ref{fig:lv:mission_preformance:ras_velocity}
\ref{fig:lv:mission_preformance:ras_accel}
\ref{lv-differences-in-results}
\ref{subsec:lv:mission-performance-predictions:ads_effect}
\ref{tab:lv:mission_preformance:ads-rationale}
\ref{tab:lv:mpp:ads_correction}
\ref{subsec:lv:mission-performance-predictions:stability-analysis}
\ref{subsubsec:lv:mission-performance-predictions:stability-analysis:openrocket-stability-predictions}
\ref{tab:lv:mpp:or_stability_analysis}
\ref{fig:lv:mission_preformance:or_stability}
\ref{fig:lv:mission_preformance:or_cp_cg}
\ref{subsubsec:lv:mission-performance-predictions:stability-analysis:rasaeroii-stability-predictions}
\ref{tab:lv:mpp:ras__stability}
\ref{fig:lv:mission_preformance:ras_stability}
\ref{fig:lv:mission_preformance:ras_cp_cg}
\ref{subsubsec:lv:mission-performance-predictions:stability-analysis:differences-in-results}
\ref{subsec:lv:mission-performance-predictions:kinetic-energy-analysis}
\ref{eqn:ke}
\ref{tab:lv:mpp:burnout_mass}
\ref{subsubsec:lv:mission-performance-predictions:kinetic-energy-analysis:openrocket-ke-predictions}
\ref{tab:lv:mpp:or_main_deployment_ke_analysis}
\ref{tab:lv:mpp:or_impact_ke_analysis}
\ref{subsubsec:lv:mission-performance-predictions:kinetic-energy-analysis:hand-calculated-ke-predictions}
\ref{tab:lv:mpp:hand_calcs_main_deployment_ke}
\ref{tab:lv:mpp:hand_calcs_ke_impact_analysis}
\ref{subsubsec:lv:mission-performance-predictions:kinetic-energy-analysis:differences-in-results}
\ref{subsec:lv:mission-performance-predictions:descent-time-analysis}
\ref{subsubsec:lv:mission-performance-predictions:descent-time-analysis}
\ref{tab:lv:mpp:or_descent_time}
\ref{subsubsec:lv:mission-performance-predictions:descent-time-analysis:hand-calculated}
\ref{tab:lv:mpp:hand_calcs_descent_time}
\ref{subsubsec:lv:mission-performance-predictions:descent-time-analysis:differences-in-results}
\ref{subsec:lv:mission-performance-predictions:drift-analysis}
\ref{subsubsec:lv:mission-performance-predictions:drift-analysis:openrocket-drift-predictions}
\ref{tab:lv:mpp:or_drift_analysis}
\ref{subsubsec:lv:mission-performance-predictions:drift-analysis:hand-calculated-drift-predictions}
\ref{tab:lv:mpp:hand_calcs_drift_analysis}
\ref{subsubsec:lv:mission-performance-predictions:drift-analysis:differences-in-results}
\ref{chap:demonstration-flights}
\ref{sec:demo:flight-test-1}
\ref{fig:demo:flight-test-1:team-photo}
\ref{subsec:demo:flight-test-1:summary-of-flight-test}
\ref{tab:demo:flight-test-1:flight-test-summary}
\ref{subsec:demo:flight-test-1:flight data}
\ref{subsec:demo:flight-test-1:flight data}
\ref{fig:demo:flight-test-1:primary raw data}
\ref{tab:demo:flight-test-1:flight-data}
\ref{fig:demo:flight-test-1:as-landed:ads}
\ref{fig:demo:flight-test-1:as-landed:forward-section}
\ref{fig:demo:flight-test-1:as-landed:drogue-parachute}
\ref{fig:demo:flight-test-1:as-landed:fins}
\ref{fig:demo:flight-test-1:as-landed:main-parachute}
\ref{fig:demo:flight-test-1:as-landed:motor}
\ref{fig:demo:flight-test-1:as-landed:payload}
\ref{fig:demo:flight-test-1:as-landed}
\ref{subsubsec:demo:flight-test-1:flight-analysis:openrocket}
\ref{fig:demo:flight-test-1:openrocket:model}
\ref{fig:demo:flight-test-1:openrocket:graph}
\ref{subsec:demo:flight-test-1:successes-and-failures}
\ref{fig:demo:flight-test-1:ads-actuation-sequence:ads-actuation-1}
\ref{fig:demo:flight-test-1:ads-actuation-sequence:ads-actuation-2}
\ref{fig:demo:flight-test-1:ads-actuation-sequence:ads-actuation-3}
\ref{fig:demo:flight-test-1:ads-actuation-sequence}
\ref{fig:demo:flight-test-1:drogue-charge:main:actuation}
\ref{fig:demo:flight-test-1:drogue-charge:main:result}
\ref{fig:demo:flight-test-1:drogue-charge:main}
\ref{fig:demo:flight-test-1:drogue-charge:backup:actuation}
\ref{fig:demo:flight-test-1:drogue-charge:backup:result}
\ref{fig:demo:flight-test-1:drogue-charge:backup}
\ref{fig:demo:flight-test-1:landing:rotations:1}
\ref{fig:demo:flight-test-1:landing:rotations:2}
\ref{fig:demo:flight-test-1:landing:rotations:3}
\ref{fig:demo:flight-test-1:landing:rotations}
\ref{fig:demo:flight-test-1:landing:break:1}
\ref{fig:demo:flight-test-1:landing:break:2}
\ref{fig:demo:flight-test-1:landing:break}
\ref{subsubsec:demo:flight-test-1:flight-analysis:antenna-failure}
\ref{fig:demo:flight-test-1:antenna-failure:1}
\ref{fig:demo:flight-test-1:antenna-failure:2}
\ref{fig:demo:flight-test-1:antenna-failure}
\ref{fig:demo:flight-test-1:antenna-failure}
\ref{subsec:demo:flight-test-1:flight-analysis}
\ref{subsubsec:demo:flight-test-1:flight-analysis:flight-data-error}
\ref{tab:demo:flight-test-1:flight-analysis:simulation-vs-actual}
\ref{subsubsec:demo:flight-test-1:flight-analysis:drag-coefficient}
\ref{subsubsec:demo:flight-test-1:flight-analysis:fullscale-subscale-difference}
\ref{subsubsec:demo:flight-test-1:flight-analysis:damaged-hardware}
\ref{subsubsec:demo:flight-test-1:flight-analysis:off-nominal-events}
\ref{sec:demo:planned-test-1}
\ref{chap:project-plan}
\ref{sec:project-plan:testing}
\ref{subsec:project-plan:testing:launch-vehicle}
\ref{subsec:project-plan:testing:nasa-stemcraft-payload}
\ref{subsec:project-plan:testing:ads-secondary-payload}
\ref{sec:project-plan:requirements-compliance}
\ref{subsec:project-plan:nasa-derived-requirements}
\ref{subsec:project-plan:team-derived-requirements}
\ref{tab:budget:Subscale}
\ref{tab:fmea:integration}
\ref{tab:budget:safety}
\ref{tab:requirements:nasa-specified-general-requirements}
\ref{tab:budget:payload}
\ref{tab:ads:budget}
\ref{tab:fmea:nasa-payload}
\ref{tab:changes:frr:ads-payload}
\ref{tab:budget:lv}
\ref{tab:u-bolt-tensile-test}
\ref{tab:vehicle-6dof-data-demonstration}
\ref{tab:requirements:team-derived-recovery-requirements}
\ref{tab:fmea:launch-vehicle}
\ref{tab:requirements:nasa-specified-vehicle-requirements}
\ref{tab:budget:stem-engagement}
\ref{tab:transmit-range}
\ref{tab:requirements:nasa-specified-payload-requirements}
\ref{tab:budget:travel}
\ref{tab:requirements:nasa-specified-safety-requirements}
\ref{tab:vehicle-recovery-ejection-charge-demonstration}
\ref{tab:requirements:nasa-specified-recovery-requirements}
\ref{tab:fmea:ads-payload}
\ref{tab:ads-timing-demonstration}
\ref{tab:ads-compression-test}
\ref{tab:ads-tension-test}
\ref{tab:flap-demonstration}
\ref{tab:flap-deformation-test}
\ref{tab:altimeter-accuracy-test}
\ref{tab:actuation-accuracy-test}
\ref{tab:requirements:team-derived-ads-requirements}
\ref{tab:fin-bending-strength-test}
\ref{tab:fin-swap-demonstration}
\ref{tab:booster-mass-test}
\ref{tab:fin-mass-demonstration}
\ref{tab:vehicle-compression-and-tensile-strength-demonstration}
\ref{tab:vehicle-bending-strength-demonstration}
\ref{tab:vehicle-rf-signal-transmission-demonstration}
\ref{tab:vehicle-ballast-weight-demonstration}
\ref{tab:vehicle-ballast-retention-demonstration}
\ref{tab:requirements:team-derived-vehicle-requirements}
\ref{tab:transmit-range}
\ref{tab:stemcraft-cg}
\ref{tab:stemcraft-drop}
\ref{tab:antenna-omni-directionality}
\ref{tab:antenna-resoce}
\ref{tab:antenna-impedance}
\ref{tab:stemcraft-drop}
\ref{tab:antenna-swr}
\ref{tab:requirements:team-derived-payload-requirements}
\ref{tab:changes:frr:project-plan}
\ref{tab:safety:recovery_operations}
\ref{tab:safety:pad_operations}
\ref{tab:safety:l-1_ejection_charge_preparation}
\ref{tab:safety:recovery_operations}
\ref{tab:safety:risks:launch}
\ref{tab:safety:risks:environmental}
\ref{tab:stemcraft-pcb-continuity}
\ref{tab:standby-battery-capacity}
\ref{tab:transmit-range}
\ref{tab:stemcraft-drop}
\ref{tab:antenna-omni-directionality}
\ref{tab:antenna-impedance}
\ref{tab:antenna-resoce}
\ref{tab:antenna-swr}
\ref{tab:stemcraft-cg}
\ref{tab:stemcraft-pcb-pull-pin-swtich-power-draw}
\ref{tab:stemcraft-pcb-voltage-step-down}
\ref{tab:stemcraft-pcb-voltage-divider}
\ref{tab:stemcraft-pcb-lightaprs-transmission}
\ref{tab:stemcraft-pcb-debugging-unit-activation}
\ref{tab:stemcraft-pcb-sensing-unit-transmission}
\ref{tab:stemcraft-pcb-lora}
\ref{tab:safety:risks:proposal}
\ref{tab:budget:project}
\ref{tab:ads-timing-demonstration}
\ref{tab:ads-compression-test}
\ref{tab:ads-tension-test}
\ref{tab:flap-flight-demonstration}
\ref{tab:flap-load-test}
\ref{tab:altimeter-accuracy-test}
\ref{tab:actuation-accuracy-test}
\ref{tab:safety:l-1_drogue_parachute_preparation}
\ref{tab:safety:l-1_main_parachute_preparation}
\ref{tab:safety:l-1_ejection_charge_preparation}
\ref{tab:safety:l-1_avionics_checkout}
\ref{tab:safety:l-1_vehicle_inspection}
\ref{tab:safety:l-0_stemcraft_payload_integration}
\ref{tab:safety:l-0_ads_payload_preparation}
\ref{tab:safety:l-0_motor_assembly}
\ref{tab:safety:l-0_avionics_checkout}
\ref{tab:safety:l-0_final_vehicle_integration}
\ref{tab:safety:pad_operations}
\ref{tab:safety:recovery_operations}
\ref{tab:safety:l+1_vehicle_cleaning}
\ref{tab:safety:troubleshooting_(catchall)}
\ref{tab:changes:frr:nasa-payload}
\ref{tab:testing:shock-cord-tensile-test}
\ref{tab:shock-cord-tensile-test}
\ref{tab:u-bolt-tensile-test}
\ref{tab:recovery-ejection-demonstration}
\ref{tab:fin-bending-strength-test}
\ref{tab:fin-swap-demonstration}
\ref{tab:fin-clamp-infill-pattern-test}
\ref{tab:fin-mass-demonstration}
\ref{tab:booster-mass-test}
\ref{tab:vehicle-compression-and-tensile-strength-demonstration}
\ref{tab:vehicle-bending-strength-demonstration}
\ref{tab:vehicle-rf-signal-transmission-demonstration}
\ref{tab:vehicle-ballast-weight-demonstration}
\ref{tab:vehicle-ballast-retention-demonstration}
\ref{tab:vehicle-recovery-ejection-charge-demonstration}
\ref{tab:vehicle-6dof-data-demonstration}
\ref{tab:camera-power-test}
\ref{tab:onboard-video-structural-integrity-demonstration}
\ref{tab:camera-temperature-functionality-demonstration}
\ref{tab:camera-shear-stress-demonstration}
\ref{tab:pad-stay-time-demonstration}
\ref{tab:requirements:nasa-specified-final-flight-requirements}
\ref{tab:safety:risks:project}
\ref{tab:safety:l-0_stemcraft_payload_integration}
\ref{tab:safety:l-0_ads_payload_preparation}
\ref{tab:safety:risks:manufacturing}