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German V/STOL Fighter Program: A Quest for Survivability in a Theater Nuclear Environment [Pehme köide]

  • Formaat: Paperback / softback, 75 pages, kõrgus: 230 mm, Illustrations
  • Ilmumisaeg: 30-Jun-1997
  • Kirjastus: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1563472473
  • ISBN-13: 9781563472473
Teised raamatud teemal:
German V/STOL Fighter Program: A Quest for Survivability in a Theater Nuclear EnvironmentSuurem pilt
  • Formaat: Paperback / softback, 75 pages, kõrgus: 230 mm, Illustrations
  • Ilmumisaeg: 30-Jun-1997
  • Kirjastus: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1563472473
  • ISBN-13: 9781563472473
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781563472473.html
This case study examines the German VTOL fighter and strike aircraft development efforts, the VJ 101 and the VAK 191B programmes. The VJ 101C and the VAK 191B design approaches are described and the results of their flight-test efforts are summarized.
PREFACE XI
PART I. VJ 101C SUPERSONIC FIGHTER/ INTERCEPTOR 1(40)
I. OVERVIEW
3(1)
II. GERMAN V/STOL FIGHTER INITIATIVE
3(1)
III. SIMULTANEOUS U.S. AIR FORCE VTOL FIGHTER DEVELOPMENT
4(3)
A. Background
4(2)
B. Bell XF-109 Supersonic VTOL Fighter
6(1)
IV. VJ 101C SUPERSONIC V/STOL RESEARCH AIRCRAFT
7(16)
A. Development/Risk Reduction Approach
7(1)
B. VJ 101C Flight Demonstrator Approach
7(1)
C. Ground/Hover Testbeds
8(1)
1. Wippe
8(1)
2. VJ 101C Hover Rig
8(1)
D. VJ 101C VTOL Research Aircraft Description
9(12)
1. Type
9(2)
2. Wings
11(1)
3. Fuselage
11(1)
4. Landing Gear
12(1)
5. Propulsion System
12(1)
6. Wingtip Engine Nacelles
13(2)
7. RB.145 Engine
15(2)
8. Integrated Flight and Propulsion Control System for V/STOL Flight
17(1)
9. Conventional Aerodynamic Flight Controls
18(3)
E. VJ 101C Flight Test Instrumentation
21(2)
V. VJ 101C FLIGHT TEST PROGRAM AND RESULTS
23(12)
A. Captive Hover Rig Testing
23(1)
B. Free-Flight Hover Rig Testing
23(1)
C. VJ 101C Captive Testing
24(1)
D. Initial Hovering Free Flights
25(2)
E. Transition to/from Vertical Flight
27(1)
F. VJ 101C and Exhaust Gas Effects
27(3)
G. Vertical Takeoff and Landing Techniques
30(1)
H. Expansion of the Flight Envelope
31(1)
I. Supersonic Flight
31(1)
J. Loss of the VJ 101C X1
31(1)
K. Afterburner Issues and the VJ 101C X2
32(1)
L. Elevated Platform Testing
33(2)
M. VJ 101C Conclusion
35(1)
VI. VJ 101D: THE PLANNED "DEFINITIVE" DEVELOPMENT
35(4)
A. VJ 101D Design Concept
35(1)
B. VJ 101D Propulsion System
36(2)
1. RB.153 Lift/Cruise Engine
36(2)
2. RB.162-31 Lift Engine
38(1)
C. VJ 101D Project Cancellation
38(1)
VII. SUMMARY
39(2)
APPENDIX A: VJ 101 PROGRAM CHRONOLOGY
40(1)
PART II. GERMAN VAK 191B TRANSONIC VTOL STRIKE FIGHTER 41(28)
I. OVERVIEW
43(1)
II. VAK 191B PROGRAM DISCUSSION
43(8)
A. Initial Design Studies
43(2)
B. NATO Requirement
45(1)
C. VAK 191 Competition
46(4)
D. Change in Project Focus
50(1)
III. VAK 191B AIRCRAFT DESCRIPTION
51(3)
A. Aircraft
51(1)
B. Propulsion System
52(2)
C. Flight Control System
54(1)
IV. VAK 191B FLIGHT TEST PROGRAM AND RESULTS
54(12)
A. Preliminary Ground and Captive Testing
55(4)
B. Conventional Takeoff and Landing Performance
59(1)
C. V/STOL Performance
59(3)
1. Hover
59(2)
2. Vertical Takeoff
61(1)
3. STOL Takeoff
61(1)
4. Transition Flight
61(1)
D. Conventional Flight
62(1)
E. Joint U.S. Navy-German VAK 191B V/STOL Research Investigation
62(4)
V. VAK 191B OBSERVATIONS
66(1)
VI. SUMMARY
67(2)
APPENDIX A: VAK 191B PROPULSION SYSTEM 69(2)
Rolls-Royce/MTU RB.193-12 Lift/Cruise Engine 69(1)
Rolls-Royce RB.162-81 Lift Engine 70(1)
APPENDIX B: VAK 191B PROGRAM CHRONOLOGY 71(1)
REFERENCES 72(1)
ADDITIONAL READING 73