Sounding Rocket Program Handbook
<span class="Apple-style-span" style="line-height: normal;">Sounding Rocket Program Handbook**** Hidden Message *****</span> <div>Rocket Program Handbook</div><div>Suborbital Projects and Operations Directorate</div><div>Sounding Rockets Program Office</div><div>National Aeronautics and Space Administration</div><div>Goddard Space Flight Center</div><div>Wallops Flight Facility</div><div>Wallops Island, Virginia 23337</div><div>July 2001</div><div>i</div><div>Preface</div><div>This Handbook describes the capabilities of the Sounding Rocket program, the design and</div><div>technology applications used by that program, and the processes established to integrate the</div><div>customer (principal investigator/program user/scientist/experimenter) into the mission team</div><div>to ensure the highest probability of a successful project.</div><div>Neither the United States Government nor any person acting on the behalf of the Unites</div><div>States Government assumes any liability resulting from the use of information contained in</div><div>this document or warrants that the use will be free from privately owned rights.</div><div>The use of a company name does not imply approval or recommendation of the product to</div><div>the exclusion of others that may also be suitable.</div><div>ii</div><div>SOUNDING ROCKET PROGRAM HANDBOOK</div><div>TABLE OF CONTENTS</div><div>PREFACE</div><div>SECTION 1: THE NASA SOUNDING ROCKET PROGRAM (NSRP) 1</div><div>1.1 THE PROGRAM: 1959 - THE PRESENT 1</div><div>1.2 NASA ORGANIZATIONAL RESPONSIBILITIES 2</div><div>1.2.1 PROGRAM MANAGEMENT 3</div><div>1.2.2 SOUNDING ROCKET WORKING GROUP (SRWG) 3</div><div>1.3 SOUNDING ROCKET PROGRAM CUSTOMER’S ROLE 3</div><div>1.3.1 PHILOSOPHY 3</div><div>1.3.2 PAYLOAD AND INSTRUMENTATION 4</div><div>1.4 SOUNDING ROCKET PROJECT SUPPORT ELEMENTS 4</div><div>1.4.1 PROGRAM-PROVIDED SUPPORT SERVICES 5</div><div>SECTION 2: THE SOUNDING ROCKET FLIGHT PROJECT 12</div><div>2.1 THE MISSION INITIATION CONFERENCE (MIC) 13</div><div>2.2 THE REQUIREMENTS DEFINITION MEETING (RDM) 16</div><div>2.3 THE DESIGN REVIEW (DR) 16</div><div>2.4 PAYLOAD FABRICATION AND PRE-INTEGRATION TESTING 19</div><div>2.5 PRE-INTEGRATION REVIEW 19</div><div>2.6 PAYLOAD INTEGRATION AND TESTING 20</div><div>2.6.1 PRE_INTEGRATION CHECKOUT 20</div><div>2.6.2 PAYLOAD INTEGRATION 21</div><div>2.6.3 ACCEPTANCE TESTING 21</div><div>2.6.4 WAIVERS 21</div><div>2.6.5 FINAL CHECKOUT 22</div><div>2.6.6 INTEGRATION AND TEST SCHEDULING 22</div><div>iii</div><div>2.7 MISSION READINESS REVIEW (MRR) 22</div><div>2.8 LAUNCH OPERATIONS 23</div><div>2.8.1 FLIGHT REQUIREMENTS PLAN 23</div><div>2.8.2 OPERATIONS AND SAFETY DIRECTIVE (OSD) 24</div><div>2.8.3 OPERATIONAL SAFETY 24</div><div>2.9 POST-LAUNCH ACTIVITIES 24</div><div>2.9.1 QUICK LOOK REPORTS 24</div><div>2.9.2 PRELIMINARY POST-FLIGHT REPORT 24</div><div>2.9.3 CUSTOMER'S WRITTEN RESPONSE 25</div><div>2.9.4 POST FLIGHT CONFERENCE 25</div><div>2.9.5 POST FLIGHT DATA 25</div><div>2.10 MISSION SUCCESS/FAILURE 25</div><div>2.10.1 ANOMALY INVESTIGATION BOARD (AIB) 26</div><div>2.10.2 IN-FLIGHT ANOMALIES 26</div><div>2.10.3 AIB ACTION ITEM - RECOMMENDATION IMPLEMENTATION TEAM 26</div><div>2.11 THE MISSION CLOSE-OUT REPORT 27</div><div>SECTION 3: SOUNDING ROCKET LAUNCH VEHICLES & PERFORMANCE CAPABILITIES 28</div><div>3.1 NASA MISSION DESIGNATION SYSTEM 28</div><div>3.2 NASA SOUNDING ROCKETS 28</div><div>3.2.1 PERFORMANCE CHARACTERISTICS 28</div><div>3.3 BOOST GUIDANCE SYSTEMS (BGS) 32</div><div>3.3.1 OPERATION OF THE S-19 BOST GUIDANCE SYSTEM 33</div><div>SECTION 4: SOUNDING ROCKET PAYLOAD DESIGN CONSIDERATIONS 35</div><div>4.1 PAYLOAD DESIGN 35</div><div>4.2 FLIGHT PERFORMANCE 36</div><div>4.2.1 MECHANICAL LOADS AND VIBRATION 36</div><div>4.2.2 THERMAL CONSIDERATIONS 37</div><div>iv</div><div>4.2.3 VACUUM AND OUT-GASSING 37</div><div>4.2.4 AERODYNAMIC DESIGN FACTORS 38</div><div>4.3 OTHER PAYLOAD DESIGN CONSIDERATIONS 38</div><div>4.3.1 ACCESSIBILITY 38</div><div>4.3.2 AVAILABILITY OF PARTS 38</div><div>4.3.3 DYNAMIC BALANCE 38</div><div>4.3.4 COST 38</div><div>4.3.5 REDUNDANCY 38</div><div>4.3.6 WEIGHT 39</div><div>4.3.7 TESTING 39</div><div>SECTION 5: PAYLOAD SYSTEMS 40</div><div>5.1 TELEMETRY SYSTEMS 40</div><div>5.1.1 DATA TRANSMISSION SYSTEMS 41</div><div>5.1.2 PCM/FM SYSTEMS 41</div><div>5.1.3 SPARCS (WFF87) ENCODER SYSTEMS 42</div><div>5.1.4 FM/FM SYSTEMS 42</div><div>5.1.5 PCM VERSUS FM 42</div><div>5.2 ATTITUDE INSTRUMENTATION SYSTEMS 43</div><div>5.2.1 MAGNETOMETER 43</div><div>5.2.2 ATTITUDE GYROSCOPE 44</div><div>5.2.3 SOLAR/LUNAR SENSORS 44</div><div>5.2.4 HORIZON SENSOR 45</div><div>5.2.5 TELEVISION CAMERAS 45</div><div>5.2.6 FILM CAMERAS 45</div><div>5.2.7 RATE SENSOR 45</div><div>5.3 TRANSMITTERS 46</div><div>5.4 COMMAND SYSTEMS 46</div><div>v</div><div>5.5 TELEMETRY ANTENNAS 47</div><div>5.6 INSTRUMENTATION AND EXPERIMENT POWER SUPPLY 47</div><div>5.6.1 SILVER ZINC CELLS 48</div><div>5.6.2 NICKEL CADMIUM 48</div><div>5.6.3 VOLTAGE OUTPUT 48</div><div>5.6.4 HEATERS 49</div><div>5.6.5 SWITCHING 49</div><div>5.6.6 PYROTECHNIC POWER SUPPLY 49</div><div>5.7 IN-FLIGHT EVENT TIMING SYSTEMS 49</div><div>5.7.1 MECHANICAL TIMERS 49</div><div>5.7.2 ELECTROMECHANICAL TIMERS 49</div><div>5.7.3 ELECTRONIC TIMERS 50</div><div>5.7.4 BAROMETRIC SWITCHES 50</div><div>5.8 TRACKING SYSTEMS 50</div><div>5.8.1 RADAR TRANSPONDERS 50</div><div>5.8.2 GLOBAL POSITIONING SYSTEM (GPS) 51</div><div>5.8.3 MAGNETIC CALIBRATION FACILITY 52</div><div>5.9 MECHANICAL SYSTEMS AND MECHANISMS 52</div><div>5.9.1 NOSE CONES 52</div><div>5.9.2 STRUCTURES AND SKINS 53</div><div>5.9.3 VACUUM DOORS 53</div><div>5.9.4 DEPLOYMENT MECHANISMS 53</div><div>5.9.5 VACUUM/WATER SEALING 53</div><div>5.9.6 MISCELLANEOUS HARDWARE 53</div><div>5.9.7 DESPIN SYSTEMS 53</div><div>5.10 RECOVERY SYSTEMS 54</div><div>5.10.1 LAND 54</div><div>vi</div><div>5.10.2 WATER 54</div><div>5.10.3 RECOVERY AIDS 54</div><div>5.11 HIGH ALTITUDE DECELERATORS 55</div><div>5.12 ATTITUDE CONTROL SYSTEMS 55</div><div>SECTION 6: THE SOLAR POINTING ATTITUDE ROCKET CONTROL SYSTEM (SPARCS) 57</div><div>6.1 SPARCS ATTITUDE CONTROL SYSTEM AND COMMAND UP-LINK 58</div><div>6.1.1 TARGETING 58</div><div>6.1.2 ACCURACY 58</div><div>6.1.3 SIZE/WEIGHT 58</div><div>6.1.4 AIRBORNE REAL-TIME COMMAND UPLINK 58</div><div>6.1.5 SPARCS COMMAND SYSTEMS (SCS) 59</div><div>6.2 INSTRUMENTATION (TELEMETRY) 59</div><div>6.3 THE WSMR PAYLOAD INTEGRATION FACILITIES 60</div><div>6.3.1 THE VIBRATION FACILITY 60</div><div>6.3.2 DYNAMIC BALANCE (ON MRC CORPORATION MACHINE) 60</div><div>6.3.3 MOMENT OF INERTIA - PITCH/YAW & ROLL 61</div><div>6.3.4 CENTER OF GRAVITY - PITCH/YAW & ROLL 61</div><div>6.3.5 BEND TEST 62</div><div>6.3.6 VACUUM SYSTEMS 62</div><div>6.3.7 MAGNETIC CALIBRATION FACILITY 62</div><div>6.3.8 DARK ROOM 62</div><div>6.3.9 FACILITY (N-200) CLEANLINESS 62</div><div>6.3.10 TARGETING 63</div><div>6.3.11 OPTICS CAPABILITIES 63</div><div>SECTION 7: ENVIRONMENTAL TESTING POLICIES 64</div><div>7.1 GENERAL REQUIREMENTS 64</div><div>7.1.1 QUALIFICATION TESTING 64</div><div>vii</div><div>7.1.2 ACCEPTANCE TESTING 64</div><div>7.1.3 PRINCIPAL INVESTIGATOR TESTING 64</div><div>7.1.4 TEST PLAN 64</div><div>7.2 TESTING EQUIPMENT AND CAPABILITIES 65</div><div>7.2.1 MASS PROPERTIES MEASUREMENT SYTEMS WFF/WSMR 65</div><div>7.2.2 STATIC AND DYNAMIC BALANCING MACHINE (WFF) 66</div><div>7.2.3 SHAKERS (WFF/WSMR) 67</div><div>7.2.4 VACUUM CHAMBERS (WFF/WSMR) 68</div><div>7.2.5 BEND TEST FIXTURES (WFF/WSMR) 70</div><div>7.2.6 SPIN DEPLOYMENT AND SEPARATION EQUIPMENT WFF 70</div><div>7.2.7 CENTRIFUGE MACHINE (WFF) 71</div><div>7.2.8 MAGNETIC TEST FACILITY (WFF) 71</div><div>7.2.9 SPIN BALANCE FACILITY (WFF) 72</div><div>7.3 PAYLOAD TESTING 74</div><div>7.3.1 STATIC AND DYNAMIC BALANCE 74</div><div>7.3.2 BEND TEST 74</div><div>7.3.3 MASS PROPERTIES 75</div><div>7.3.4 VIBRATION 75</div><div>7.3.5 WAIVERS 78</div><div>7.3.6 TEST TIMES 78</div><div>7.4 COMPONENT TESTING 78</div><div>SECTION 8: NASA/GSFC/WFF SAFETY POLICY AND RESPONSIBILITIES 79</div><div>8.1 SAFETY POLICY 80</div><div>8.2 THE RANGE SAFETY ORGANIZATION 81</div><div>8.2.1 SAFETY RESPONSIBILITIES OF THE MISSION MANAGER 81</div><div>8.2.2 SAFETY RESPONSIBILITIES OF THE PRINCIPAL INVESTIGATOR 82</div><div>8.3 GROUND SAFETY PLAN 83</div><div>viii</div><div>8.4 FLIGHT SAFETY PLAN 84</div><div>8.4.1 IMPACT CRITERIA 84</div><div>8.4.2 OVERFLIGHT CRITERIA 85</div><div>8.4.3 FLIGHT TERMINATION CRITERIA 85</div><div>8.4.4 FLIGHT TERMINATION SYSTEM DESIGN REQUIREMENTS 85</div><div>8.4.5 FLIGHT PLANNING CRITERIA 85</div><div>8.4.6 RANGE CLEARANCE CRITERIA FOR GSFC/WFF LAUNCH RANGE 85</div><div>8.4.7 OPERATIONAL PROCEDURES 86</div><div>8.5 SAFETY ANALYSIS REPORT 86</div><div>SECTION 9: LAUNCH OPERATIONS 87</div><div>9.1 LAUNCH RANGES 87</div><div>9.2 LAUNCH OPERATIONS 89</div><div>9.2.1 RULES TO REMEMBER 89</div><div>9.2.2 ROLE OF THE MISSION MANAGER 90</div><div>9.2.3 THE FLIGHT REQUREMENTS PLAN 90</div><div>9.2.4 TEST AND EVALUATION 90</div><div>9.2.5 THE FIELD SCHEDULE 90</div><div>9.2.6 THE PREFLIGHT CONFERENCE 91</div><div>9.2.7 RECOVERY 91</div><div>9.2.8 POST-FLIGHT CONFERENCE 91</div><div>9.3 FOREIGN RANGES 91</div><div>9.3.1 EXPERIMENTAL TECHNIQUES 92</div><div>9.3.2 TRAVEL & LODGING 92</div><div>9.3.3 ACCESS 92</div><div>9.3.4 FOREIGN NATIONALS 92</div><div>9.3.5 EXPORT CONTROL 93</div><div>9.3.6 POSTAL SERVICE 93</div><div>ix</div><div>9.3.7 SHIPPING 93</div><div>9.4 MOBILE RANGE OPERATIONS 93</div><div>9.4.1 REMOTE LOCATIONS 97</div><div>9.4.2 HARSH ENVIRONMENT 97</div><div>9.4.3 LIMITED TECHNICAL FACILITIES 97</div><div>9.4.4 LIMITED COMMUNICATIONS 98</div><div>SECTION 10: DATA PROCESSING AND ANALYSIS 99</div><div>10.1 COMPUTER SYSTEMS 99</div><div>10.1.1 REAL TIME COMPTUER SYSTEM (RTCS) 99</div><div>10.1.2 DATA REDUCTION COMPUTER SYSTEM (DRCS) 99</div><div>10.1.3 ENGINEERING COMPUTER SYSTEM (ECS) 100</div><div>10.1.4 LAUNCH STATUS REVIEW SYSTEM (LSRS) 100</div><div>10.1.5 SPECIAL PURPOSE COMPUTERS 101</div><div>10.1.6 DIGITAL TELEMETRY FACILITY 101</div><div>10.2 OBTAINING DATA PROCESSING AND ANALYSIS SUPPORT 101</div><div>10.2.1 FLIGHT REQUIREMENTS PLAN (FRP) 101</div><div>10.2.2 INSTRUMENTATION (TELEMETRY) 102</div><div>10.2.3 NON-STANDARD USER REQUIREMENTS 102</div><div>10.2.4 POSITIONAL DATA POLICY 102</div><div>10.2.5 DATA DISSEMINATION 102</div><div>10.2.6 DATA RETENTION 103</div><div>SECTION 11: WALLOPS FLIGHT FACILITY 104</div><div>11.1 WFF SOUNDING ROCKET PROGRAM SUPPORT FACILITIES 106</div><div>11.1.1 ENGINEERING SUPPORT FACILITIES 107</div><div>11.1.2 PAYLOAD INTEGRATION LABORATORY 107</div><div>11.1.3 ENVIRONMENTAL TESTING LABORATORY 108</div><div>11.14 PAYLOAD CONSTRUCTION 111</div><div>x</div><div>11.1.5 COMPUTER SUPPORT 112</div><div>11.1.6 RANGE OPERATIONS 112</div><div>11.2 WORKING AT WALLOPS – RULES, REGULATIONS, AND LOGISTICS 114</div><div>11.2.1 ACCESS 114</div><div>11.2.2 ACCOMMODATIONS 114</div><div>11.2.3 WFF - SAFETY RULES AND REGULATIONS 116</div><div>11.2.4 SHIPPING/RECEIVING & TRANSPORTATION OF SOUNDING</div><div>ROCKET COMPONENTS 117</div><div>11.3 FOREIGN NATIONALS 118</div><div>APPENDICES</div><div>APPENDIX A: PRINCIPAL INVESTIGATOR'S DATA PACKAGE FOR MISSION</div><div>INITIATION CONFERENCE (MIC) A-120</div><div>APPENDIX B RDM DATA PACKAGE B-123</div><div>APPENIX C PRINCIPAL INVESTIGATOR'S DATA PACKAGE FOR A DESIGN</div><div>REVIEW C-129</div><div>APPENDIX D PRINCIPAL INVESTIGATOR'S DATA PACKAGE FOR A MISSION</div><div>READINESS REVIEW D-130</div><div>APPENDIX E PRELIMINARY POST-FLIGHT REPORT OUTLINE E-132</div><div>APPENDIX F NASA SOUNDING ROCKET DESCRIPTIONS AND FLIGHT</div><div>PERFORMANCE CHARACTERISTICS F-135</div><div>F.1 SUPER ARCAS LAUNCH VEHICLE (15.XXX) F-136</div><div>F.2 BLACK BRANT V LAUNCH VEHICLE (21.XXX) F-138</div><div>F.3 NIKE-BLACK BRANT V B/C LAUNCH VEHICLE (27.XXX) F-141</div><div>F.4 TERRIER-MALEMUTE LAUNCH VEHICLE (29.XXX) F-144</div><div>F.5 ORION LAUNCH VEHICLE (30.XXX) F-146</div><div>F.6 NIKE-ORION LAUNCH VEHICLE (31.XXX) F-148</div><div>F.7 TAURUS-ORION LAUNCH VEHICLE (33.XXX) F-150</div><div>F.8 BLACK BRANT X LAUNCH VEHICLE (35.XXX) F-152</div><div>xi</div><div>F.9 TERRIER-BLACK BRANT VC LAUNCH VEHICLE (BLACK</div><div>BRANT IX, 36.XXX) F-154</div><div>F.10 VIPER DART LAUNCH VEHICLE (37.XXX) F-159</div><div>F.11 BLACK BRANT XI LAUNCH VEHICLE (39.XXX) F-162</div><div>F.12 BLACK BRANT XII LAUNCH VEHICLE (40.XXX) F-165</div><div>F.13 TERRIER-IMPROVED ORION (41.XXX) F-168</div><div>F.14 TERRIER LYNX (42.XXX) F-170</div><div>APPENDIX G PCM/FM AND FM/FM TELEMETRY SYSTEMS G-172</div><div>G.1 VECTOR MMP-900 PCM SYSTEM G-172</div><div>G.2 SPARCS AND THE PSL WFF87 ENCODER SYSTEMS G-173</div><div>G.3 WFF93 ENCODER SYSTEM G-173</div><div>G.4 FM/FM TELEMETRY SYSTEMS G-174</div><div>APPENDIX H COMPARISON AND PERFORMANCE OF VARIOUS BATTERY SYSTEMS H-176</div><div>APPENDIX I ATTITUDE CONTROL SYSTEMS I-179</div><div>I.1 ATTITUDE CONTROL SYSTEM OVERVIEW I-179</div><div>I.2 NSROC SOLAR POINTING ATTITUDE ROCKET CONTROL</div><div>SYSTEM (VII) I-179</div><div>I.3 SPACE VECTOR CORPORATION (SVC) INERTIAL ACS I-184</div><div>I.4 SVC MAGNETIC ACS I-188</div><div>I.5 SVC RATE CONTROL SYSTEM I-191</div><div>I.6 AEROJET MARK VI ACS I-195</div><div>I.7 AEROJET MARK VID ACS I-199</div><div>APPENDIX J GSFC/WFF SAFETY DATA REQUIREMENTS J-205</div><div>PAYLOAD DESCRIPTION DATA/HAZARDOUS MATERIALS J-205</div><div>PAYLOAD DESCRIPTION DATA/RADIOACTIVE MATERIALS J-206</div><div>APPENDIX K SOUNDING ROCKET LAUNCH RANGES K-208</div><div>K.1 U.S. ARMY WHITE SANDS MISSILE RANGE K-208</div><div>K.2 POKER FLAT RESEARCH RANGE K-212</div><div>xii</div><div>K.3 ANDØYA ROCKET RANGE, NORWAY K-215</div><div>K.4 ESRANGE, SWEDEN K-218</div><div>APPENDIX L: WALLOPS FLIGHT FACILITY DIGITAL TELEMETRY SYSTEM L-221</div><div>APPENDIX M: RADAR DATA FORMAT M-224</div><div>APPENDIX N MISSION MANAGER AND SUPPORT SECTIONS (APPROVAL FOR</div><div>SOUNDING ROCKET MISSIONS) N-225</div><div>ACRONYM LIST 235</div><div>xiii</div><div>LIST OF FIGURES</div><div>FIGURE 2-1 TYPICAL SOUNDING ROCKET MISSION LIFE CYCLE 14</div><div>FIGURE 2.4-1 THE PFAFF PAYLOAD USED EXTENDED BOOMS TO</div><div>INVESTIGATE SPORADIC E EVENTS IN THE IONOSPHERE 19</div><div>FIGURE 2.4.2 MENTORED BY NSROC STAFF, UVA STUDENTS BEGIN</div><div>ELECTRICAL WIRING OF THEIR PAYLOAD AT WFF 19</div><div>FIGURE 3.2-1 NASA SOUNDING ROCKET LAUNCH VEHICLES 30</div><div>FIGURE 3.2.1-1 NASA SOUNDING ROCKET VEHICLE PERFORMANCE GRAPH 31</div><div>FIGURE 3.3.1-1A S-19 BOOST GUIDANCE SYSTEM 33</div><div>FIGURE 3.3.1-1B S-19 BOOST GUIDANCE SYSTEM 33</div><div>FIGURE 3.3.1-2 DS-19 BOOST GUIDANCE SYSTEM 34</div><div>FIGURE 5-1 PFAFF PAYLOAD 21.126 WITH BOOMS EXTENDED 40</div><div>FIGURE 5.1.1-1 TYPICAL WFF-93 PCM ENCODER 42</div><div>FIGURE 5.2.2-1 MIDAS ATTITUDE SENSOR 44</div><div>FIGURE 7.2.1-1 AIRDYNE MARK 8 MASS PROPERTIES MEASUREMENT SYSTEM 66</div><div>FIGURE S.2.2-1 GISHOLT ROCKET BALANCING MACHINE AT WFF 66</div><div>FIGURE 7.2.3-1 LING ELECTRONICS B335 THRUST AXIS SHAKER AT WFF 68</div><div>FIGURE 7.2.4-1 PV/T VACUUM CHANGER AND TENNEY SPACE SIMULATION</div><div>SYSTEM THERMAL VACUUM CHAMBER AT WFF 69</div><div>FIGURE 7.2.5-1 BEND TEST FIXTURE AT WFF 70</div><div>FIGURE 7.2.6-1 SPIN DEPLOYMENT CHAMBER AT WFF 71</div><div>FIGURE 7.2.7-1 GENISCO CENTRIFUGE MACHINE AT WFF 71</div><div>FIGURE 7.3.4-1 NEW OR MODIFIED PAYLOAD VIBRATION TESTING</div><div>FLOWCHART 76</div><div>FIGURE 7.3.4-2 REFLY PAYLOAD VIBRATION TESTING FLOW CHART 76</div><div>FIGURE 9.1-1 SOUNDING ROCKET LAUNCH SITES WORLDWIDE 89</div><div>FIGURE 9.3-1 RANGE FACILITEIS AT WOOMERA, AUSTRALIA 92</div><div>FIGURE 9.4-1 MILITARY LAUNCH AT WSMR 94</div><div>xiv</div><div>FIGURE 9.4-2 RANGE SUPPORT OPERATIONS IN SONDRE STROMFJORD,</div><div>GREENLAND 96</div><div>FIGURE 9.4-2A EXTREME CONDITIONS: SONDRE STROMFJORD, GREENLAND 96</div><div>FIGURE 9.4-2B OBSERVATIONS: NORTHERN LIGHTS AT SONDRE</div><div>STROMFJORD, GREENLAND 96</div><div>FIGURE 9.4-3 BLACK BRANT IV PAYLOAD IN WOOMERA, AUSTRALIA 97</div><div>FIGURE 11-1 WALLOPS FLIGHT FACILITY MAP 104</div><div>FIGURE 11-2 WALLOPS MAIN BASE 105</div><div>FIGURE 11-3 WALLOPS ISLAND 105</div><div>FIGURE 11-4 WALLOPS MAINLAND 106</div><div>FIGURE 11.1.2-1 PLASMA PHYSICS PAYLOAD DURING PAYLOAD INTEGRATION 107</div><div>FIGURE 11.1.2-2 ASTROPHYSICS PAYLOAD DURING PAYLOAD INTEGRATION 108</div><div>FIGURE 11.1.3-1 ASTROPHYSICS PAYLOAD UNDERGOING LATERAL VIBRATION</div><div>TESTING 109</div><div>FIGURE 11.1.4-1 WALLOPS FLIGHT FACILITY MACHINE SHOP – ELECTRICAL</div><div>SECTION 112</div><div>FIGURE 11.1.4-2 A NOSE CONE IS STREAMLINED IN THE MACHINE SHOP 112</div><div>FIGURE 11.1.6-1 WFF FIXED RADAR SYSTEM 113</div><div>FIGURE F.1-1 SUPER ARCAS LAUNCH VEHICLE</div> Sounding Rocket Program Handbook 好的资料！好的资料！
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