Uncategorized files

Showing below up to 50 results in range #151 to #200.

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  FIGURE 7-10. Main-Parachute Assembly..jpg 602 × 294; 31 KB
  
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  FIGURE 7-11. Vent-Tape Geometry..jpg 235 × 182; 6 KB
  
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  FIGURE 7-12. Bench Check on Gore Fullness..jpg 589 × 192; 16 KB
  
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  FIGURE 7-13. Gore Layout for Gore Dimensions..jpg 317 × 284; 15 KB
  
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  FIGURE 7-14. Vent Construction..jpg 301 × 168; 11 KB
  
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  FIGURE 7-15. Final Gore Dimensions..jpg 251 × 409; 17 KB
  
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  FIGURE 7-15 Final Gore Dimensions.jpg 518 × 894; 69 KB
  
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  FIGURE 7-16. Pocket Band Arrangement..jpg 276 × 274; 14 KB
  
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  FIGURE 7-17. Drone Flight Envelope..jpg 448 × 343; 18 KB
  
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  FIGURE 7-18. Drogue Chute Arrangement..jpg 588 × 234; 19 KB
  
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  FIGURE 7-19. Venetian-Blind Effect of Horizontal Ribbon in a Ribbon Canopy..jpg 219 × 212; 5 KB
  
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  FIGURE 7-2. Cluster of Two 72.7-Foot-Diameter Extended-Skirt Parachutes (Drawn to Scale)..jpg 389 × 411; 20 KB
  
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  FIGURE 7-20. Canopy Gore Layout..jpg 589 × 552; 56 KB
  
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  FIGURE 7-21. Preliminary Gore Dimensions..jpg 326 × 526; 18 KB
  
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  FIGURE 7-22. Final Gore Dimensions..jpg 516 × 428; 35 KB
  
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  FIGURE 7-3. Parachute Assembly Installation and Extraction Concept..jpg 527 × 177; 21 KB
  
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  FIGURE 7-4. Determination of Equivalent Forebody Diameter..jpg 376 × 145; 11 KB
  
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  FIGURE 7-5. Extraction-Parachute Assembly..jpg 549 × 219; 17 KB
  
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  FIGURE 7-6. Pilot Chute Assembly..jpg 608 × 189; 18 KB
  
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  FIGURE 7-7. Main Parachute Assembly; Cluster of Two Parachutes..jpg 1,047 × 395; 57 KB
  
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  FIGURE 7-8. Velocity-Time Profile..jpg 604 × 245; 20 KB
  
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  FIGURE 7-9. Drag-Area-Versus-Time Profile for a Single Parachute and the Total Drone..jpg 604 × 579; 41 KB
  
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  FIGURE 8-1. Salt Drone Parachute Recovery Sequence..jpg 673 × 631; 53 KB
  
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  FIGURE 8-10. Plan Form of the 6.2-Meter Aeroconical..jpg 467 × 411; 43 KB
  
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  FIGURE 8-11. Assembly Components of the 6.2-Meter Aero conical..jpg 736 × 451; 35 KB
  
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  FIGURE 8-12. Opening Sequence of AGES Parachute Assembly..jpg 699 × 626; 41 KB
  
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  FIGURE 8-13. Side View of Escape Pole Deployed Through Side Hatch..jpg 519 × 291; 15 KB
  
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  FIGURE 8-14. Crew Bailout Mode-Crew Escape Pole..jpg 713 × 480; 38 KB
  
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  FIGURE 8-15. Navy Test Jumper Using Crew Escape Pole..jpg 598 × 525; 25 KB
  
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  FIGURE 8-15. Navy Test Jumper Using Crew Escape Pole.2.jpg 551 × 623; 133 KB
  
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  FIGURE 8-16. Parachute Extraction System for Cargo Platforms..jpg 691 × 470; 58 KB
  
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  FIGURE 8-17. Standard Airdrop Method..jpg 850 × 712; 50 KB
  
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  FIGURE 8-18. The LAPES C-130 platform Extraction System..jpg 788 × 432; 45 KB
  
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  FIGURE 8-19. High-Altitude Airdrop Resupply System (HAARS). First-Stage Configuration..jpg 530 × 513; 34 KB
  
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  FIGURE 8-2. Sequence of CL 289 Drone Recovery..jpg 836 × 626; 51 KB
  
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  FIGURE 8-20. Parachute Extraction Force and Extraction Speed vs. Time for a 35-Foot Parachute Extracting a 50,000-Pound Load..jpg 733 × 404; 27 KB
  
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  FIGURE 8-21, T-10 Paratrooper Parachute..jpg 418 × 680; 66 KB
  
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  FIGURE 8-21, T-10 Paratrooper Parachute.2.jpg 510 × 784; 167 KB
  
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  FIGURE 8-22. MC1-1B Maneuverable Parachute With Glide and Control Slots and Anti-Inversion Net.2.jpg 543 × 542; 117 KB
  
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  FIGURE 8-22. MCI-IB Maneuverable Parachute With Glide and Control Slots and Anti-Inversion Net..jpg 530 × 513; 51 KB
  
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  FIGURE 8-23. Aircraft Landing Roll as a Function of Parachute Diameter and Runway Conditions..jpg 440 × 369; 30 KB
  
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  FIGURE 8-24. B-52 With 44-Foot Diameter Landing Deceleration Parachute..jpg 584 × 267; 20 KB
  
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  FIGURE 8-24. B-52 With 44-Foot Diameter Landing Deceleration Parachute.2.jpg 614 × 244; 63 KB
  
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  FIGURE 8-25. Typical Landing Deceleration Parachute Installation..jpg 576 × 150; 15 KB
  
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  FIGURE 8-26. Typical Spin Stall Recovery Parachute Assembly and Deployment Concept..jpg 441 × 299; 23 KB
  
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  FIGURE 8-27. Deploymeny Sequence of the F-18 Spin Recovery Parachute..jpg 524 × 668; 30 KB
  
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  FIGURE 8-27. Deploymeny Sequence of the F-18 Spin Recovery Parachute.2.jpg 509 × 664; 134 KB
  
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  FIGURE 8-28. Effect or Ratio Vehicle Weight, W, to Decelerator Drag Area (CIS) on Down-Range distance, Impact Angle, and Aircraft Separation Instance..jpg 617 × 508; 39 KB
  
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  FIGURE 8-28. Effect or Ratio Vehicle Weight, W, to Decelerator Drag Area (CIS) on Down-Range distance, Impact Angle, and Aircraft Seperation Instance.2.jpg 741 × 631; 79 KB
  
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  FIGURE 8-29. Mark 83 Bomb With Ballute-Type Retarder..jpg 363 × 476; 14 KB