1
00:00:23,359 --> 00:00:24,390

the ability to

2
00:00:24,390 --> 00:00:24,400
the ability to
 

3
00:00:24,400 --> 00:00:27,029
the ability to
take off in a short distance and land in

4
00:00:27,029 --> 00:00:27,039
take off in a short distance and land in
 

5
00:00:27,039 --> 00:00:28,390
take off in a short distance and land in
a short distance

6
00:00:28,390 --> 00:00:28,400
a short distance
 

7
00:00:28,400 --> 00:00:31,349
a short distance
or vertically is something aeronautical

8
00:00:31,349 --> 00:00:31,359
or vertically is something aeronautical
 

9
00:00:31,359 --> 00:00:33,670
or vertically is something aeronautical
engineers have strived towards

10
00:00:33,670 --> 00:00:33,680
engineers have strived towards
 

11
00:00:33,680 --> 00:00:36,870
engineers have strived towards
since world war two early attempts at

12
00:00:36,870 --> 00:00:36,880
since world war two early attempts at
 

13
00:00:36,880 --> 00:00:37,190
since world war two early attempts at
this

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this
 

15
00:00:37,200 --> 00:00:41,030
this
include the autogyro the helicopter

16
00:00:41,030 --> 00:00:41,040
include the autogyro the helicopter
 

17
00:00:41,040 --> 00:00:45,910
include the autogyro the helicopter
the vertiget and other research aircraft

18
00:00:45,910 --> 00:00:45,920
the vertiget and other research aircraft
 

19
00:00:45,920 --> 00:00:48,869
the vertiget and other research aircraft
today we have machines like the v-22

20
00:00:48,869 --> 00:00:48,879
today we have machines like the v-22
 

21
00:00:48,879 --> 00:00:50,150
today we have machines like the v-22
osprey

22
00:00:50,150 --> 00:00:50,160
osprey
 

23
00:00:50,160 --> 00:00:53,270
osprey
a tilt rotor aircraft

24
00:00:53,270 --> 00:00:53,280
a tilt rotor aircraft
 

25
00:00:53,280 --> 00:00:56,150
a tilt rotor aircraft
the quiet short-haul research aircraft

26
00:00:56,150 --> 00:00:56,160
the quiet short-haul research aircraft
 

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00:00:56,160 --> 00:00:56,830
the quiet short-haul research aircraft
or

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or
 

29
00:00:56,840 --> 00:00:59,670
or
qsra and the rotor system

30
00:00:59,670 --> 00:00:59,680
qsra and the rotor system
 

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00:00:59,680 --> 00:01:03,029
qsra and the rotor system
research aircraft or rsra

32
00:01:03,029 --> 00:01:03,039
research aircraft or rsra
 

33
00:01:03,039 --> 00:01:05,429
research aircraft or rsra
which are in flight testing programs at

34
00:01:05,429 --> 00:01:05,439
which are in flight testing programs at
 

35
00:01:05,439 --> 00:01:06,710
which are in flight testing programs at
other nasa centers

36
00:01:06,710 --> 00:01:06,720
other nasa centers
 

37
00:01:06,720 --> 00:01:09,670
other nasa centers
in the united states there is one

38
00:01:09,670 --> 00:01:09,680
in the united states there is one
 

39
00:01:09,680 --> 00:01:11,990
in the united states there is one
aircraft currently being used that is a

40
00:01:11,990 --> 00:01:12,000
aircraft currently being used that is a
 

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00:01:12,000 --> 00:01:12,469
aircraft currently being used that is a
true

42
00:01:12,469 --> 00:01:12,479
true
 

43
00:01:12,479 --> 00:01:15,350
true
stovl type aircraft it is the british

44
00:01:15,350 --> 00:01:15,360
stovl type aircraft it is the british
 

45
00:01:15,360 --> 00:01:16,469
stovl type aircraft it is the british
made harrier

46
00:01:16,469 --> 00:01:16,479
made harrier
 

47
00:01:16,479 --> 00:01:19,429
made harrier
jump jet this plane is manufactured in

48
00:01:19,429 --> 00:01:19,439
jump jet this plane is manufactured in
 

49
00:01:19,439 --> 00:01:20,469
jump jet this plane is manufactured in
the united states

50
00:01:20,469 --> 00:01:20,479
the united states
 

51
00:01:20,479 --> 00:01:23,270
the united states
by mcdonnell douglas under license as

52
00:01:23,270 --> 00:01:23,280
by mcdonnell douglas under license as
 

53
00:01:23,280 --> 00:01:25,270
by mcdonnell douglas under license as
the av-8a

54
00:01:25,270 --> 00:01:25,280
the av-8a
 

55
00:01:25,280 --> 00:01:29,429
the av-8a
and av8b here at lewis research center

56
00:01:29,429 --> 00:01:29,439
and av8b here at lewis research center
 

57
00:01:29,439 --> 00:01:31,670
and av8b here at lewis research center
we are currently testing scale models of

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00:01:31,670 --> 00:01:31,680
we are currently testing scale models of
 

59
00:01:31,680 --> 00:01:32,469
we are currently testing scale models of
advanced

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00:01:32,469 --> 00:01:32,479
advanced
 

61
00:01:32,479 --> 00:01:35,590
advanced
supersonic stoval concepts hot gas

62
00:01:35,590 --> 00:01:35,600
supersonic stoval concepts hot gas
 

63
00:01:35,600 --> 00:01:36,550
supersonic stoval concepts hot gas
ingestion

64
00:01:36,550 --> 00:01:36,560
ingestion
 

65
00:01:36,560 --> 00:01:38,950
ingestion
and controls and propulsion system

66
00:01:38,950 --> 00:01:38,960
and controls and propulsion system
 

67
00:01:38,960 --> 00:01:40,230
and controls and propulsion system
technology

68
00:01:40,230 --> 00:01:40,240
technology
 

69
00:01:40,240 --> 00:01:42,870
technology
lewis's main role then is to develop

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00:01:42,870 --> 00:01:42,880
lewis's main role then is to develop
 

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00:01:42,880 --> 00:01:44,950
lewis's main role then is to develop
advanced propulsion concepts for air

72
00:01:44,950 --> 00:01:44,960
advanced propulsion concepts for air
 

73
00:01:44,960 --> 00:01:45,590
advanced propulsion concepts for air
breathing

74
00:01:45,590 --> 00:01:45,600
breathing
 

75
00:01:45,600 --> 00:01:48,230
breathing
aircraft a stovall is an air breathing

76
00:01:48,230 --> 00:01:48,240
aircraft a stovall is an air breathing
 

77
00:01:48,240 --> 00:01:49,190
aircraft a stovall is an air breathing
aircraft

78
00:01:49,190 --> 00:01:49,200
aircraft
 

79
00:01:49,200 --> 00:01:52,310
aircraft
we develop the engines we develop the

80
00:01:52,310 --> 00:01:52,320
we develop the engines we develop the
 

81
00:01:52,320 --> 00:01:54,469
we develop the engines we develop the
propulsion components that are required

82
00:01:54,469 --> 00:01:54,479
propulsion components that are required
 

83
00:01:54,479 --> 00:01:55,670
propulsion components that are required
to

84
00:01:55,670 --> 00:01:55,680
to
 

85
00:01:55,680 --> 00:01:58,469
to
power these type of aircraft there are

86
00:01:58,469 --> 00:01:58,479
power these type of aircraft there are
 

87
00:01:58,479 --> 00:02:00,870
power these type of aircraft there are
five types of propulsion concepts for

88
00:02:00,870 --> 00:02:00,880
five types of propulsion concepts for
 

89
00:02:00,880 --> 00:02:03,109
five types of propulsion concepts for
stovle type aircraft

90
00:02:03,109 --> 00:02:03,119
stovle type aircraft
 

91
00:02:03,119 --> 00:02:07,749
stovle type aircraft
vectored thrust ejector augmenter

92
00:02:07,749 --> 00:02:07,759
vectored thrust ejector augmenter
 

93
00:02:07,759 --> 00:02:11,190
vectored thrust ejector augmenter
augmented lift system lift plus

94
00:02:11,190 --> 00:02:11,200
augmented lift system lift plus
 

95
00:02:11,200 --> 00:02:14,229
augmented lift system lift plus
lift crews and the tandem fan

96
00:02:14,229 --> 00:02:14,239
lift crews and the tandem fan
 

97
00:02:14,239 --> 00:02:17,430
lift crews and the tandem fan
configuration the one that we see

98
00:02:17,430 --> 00:02:17,440
configuration the one that we see
 

99
00:02:17,440 --> 00:02:19,110
configuration the one that we see
the most of in the news today is the

100
00:02:19,110 --> 00:02:19,120
the most of in the news today is the
 

101
00:02:19,120 --> 00:02:20,550
the most of in the news today is the
harrier and that's the vector

102
00:02:20,550 --> 00:02:20,560
harrier and that's the vector
 

103
00:02:20,560 --> 00:02:22,949
harrier and that's the vector
thrust type of configuration it uses an

104
00:02:22,949 --> 00:02:22,959
thrust type of configuration it uses an
 

105
00:02:22,959 --> 00:02:24,390
thrust type of configuration it uses an
engine has four

106
00:02:24,390 --> 00:02:24,400
engine has four
 

107
00:02:24,400 --> 00:02:28,309
engine has four
variable nozzles on it that can be aimed

108
00:02:28,309 --> 00:02:28,319
variable nozzles on it that can be aimed
 

109
00:02:28,319 --> 00:02:28,710
variable nozzles on it that can be aimed
in a

110
00:02:28,710 --> 00:02:28,720
in a
 

111
00:02:28,720 --> 00:02:31,990
in a
either in the vertical direction or or

112
00:02:31,990 --> 00:02:32,000
either in the vertical direction or or
 

113
00:02:32,000 --> 00:02:34,390
either in the vertical direction or or
horizontally for forward flight each of

114
00:02:34,390 --> 00:02:34,400
horizontally for forward flight each of
 

115
00:02:34,400 --> 00:02:36,070
horizontally for forward flight each of
these systems have specific

116
00:02:36,070 --> 00:02:36,080
these systems have specific
 

117
00:02:36,080 --> 00:02:39,110
these systems have specific
advantages and disadvantages but one of

118
00:02:39,110 --> 00:02:39,120
advantages and disadvantages but one of
 

119
00:02:39,120 --> 00:02:40,470
advantages and disadvantages but one of
the main problems

120
00:02:40,470 --> 00:02:40,480
the main problems
 

121
00:02:40,480 --> 00:02:43,430
the main problems
is one of technology there are several

122
00:02:43,430 --> 00:02:43,440
is one of technology there are several
 

123
00:02:43,440 --> 00:02:45,670
is one of technology there are several
really key concepts that

124
00:02:45,670 --> 00:02:45,680
really key concepts that
 

125
00:02:45,680 --> 00:02:48,070
really key concepts that
propulsion technologies that have to be

126
00:02:48,070 --> 00:02:48,080
propulsion technologies that have to be
 

127
00:02:48,080 --> 00:02:49,270
propulsion technologies that have to be
developed

128
00:02:49,270 --> 00:02:49,280
developed
 

129
00:02:49,280 --> 00:02:52,390
developed
one of the more obvious ones is that you

130
00:02:52,390 --> 00:02:52,400
one of the more obvious ones is that you
 

131
00:02:52,400 --> 00:02:54,550
one of the more obvious ones is that you
in order to make these airplanes flyable

132
00:02:54,550 --> 00:02:54,560
in order to make these airplanes flyable
 

133
00:02:54,560 --> 00:02:56,390
in order to make these airplanes flyable
you have to get lightweight

134
00:02:56,390 --> 00:02:56,400
you have to get lightweight
 

135
00:02:56,400 --> 00:02:58,790
you have to get lightweight
propulsion systems nasa and the

136
00:02:58,790 --> 00:02:58,800
propulsion systems nasa and the
 

137
00:02:58,800 --> 00:03:00,710
propulsion systems nasa and the
department of defense have a major

138
00:03:00,710 --> 00:03:00,720
department of defense have a major
 

139
00:03:00,720 --> 00:03:03,190
department of defense have a major
activity going on to develop lightweight

140
00:03:03,190 --> 00:03:03,200
activity going on to develop lightweight
 

141
00:03:03,200 --> 00:03:04,630
activity going on to develop lightweight
high thrust await

142
00:03:04,630 --> 00:03:04,640
high thrust await
 

143
00:03:04,640 --> 00:03:07,830
high thrust await
basic engine concepts that applies to

144
00:03:07,830 --> 00:03:07,840
basic engine concepts that applies to
 

145
00:03:07,840 --> 00:03:09,430
basic engine concepts that applies to
all advanced fighters

146
00:03:09,430 --> 00:03:09,440
all advanced fighters
 

147
00:03:09,440 --> 00:03:11,430
all advanced fighters
in the case of stovall then there's some

148
00:03:11,430 --> 00:03:11,440
in the case of stovall then there's some
 

149
00:03:11,440 --> 00:03:13,110
in the case of stovall then there's some
other special issues

150
00:03:13,110 --> 00:03:13,120
other special issues
 

151
00:03:13,120 --> 00:03:15,589
other special issues
one is the lift concepts themselves the

152
00:03:15,589 --> 00:03:15,599
one is the lift concepts themselves the
 

153
00:03:15,599 --> 00:03:16,949
one is the lift concepts themselves the
ejector system

154
00:03:16,949 --> 00:03:16,959
ejector system
 

155
00:03:16,959 --> 00:03:20,949
ejector system
the raw system lift engines

156
00:03:20,949 --> 00:03:20,959
the raw system lift engines
 

157
00:03:20,959 --> 00:03:23,430
the raw system lift engines
those all have to be the technologies

158
00:03:23,430 --> 00:03:23,440
those all have to be the technologies
 

159
00:03:23,440 --> 00:03:25,270
those all have to be the technologies
associated with those concepts have to

160
00:03:25,270 --> 00:03:25,280
associated with those concepts have to
 

161
00:03:25,280 --> 00:03:26,710
associated with those concepts have to
be developed

162
00:03:26,710 --> 00:03:26,720
be developed
 

163
00:03:26,720 --> 00:03:28,149
be developed
specifically here at lewis we're

164
00:03:28,149 --> 00:03:28,159
specifically here at lewis we're
 

165
00:03:28,159 --> 00:03:30,630
specifically here at lewis we're
investigating the ejector concept

166
00:03:30,630 --> 00:03:30,640
investigating the ejector concept
 

167
00:03:30,640 --> 00:03:34,070
investigating the ejector concept
as part of our current program um

168
00:03:34,070 --> 00:03:34,080
as part of our current program um
 

169
00:03:34,080 --> 00:03:39,589
as part of our current program um
then additional items uh on the list uh

170
00:03:39,589 --> 00:03:39,599
then additional items uh on the list uh
 

171
00:03:39,599 --> 00:03:42,390
then additional items uh on the list uh
a lot of these concepts have uh complex

172
00:03:42,390 --> 00:03:42,400
a lot of these concepts have uh complex
 

173
00:03:42,400 --> 00:03:43,830
a lot of these concepts have uh complex
internal ducting that

174
00:03:43,830 --> 00:03:43,840
internal ducting that
 

175
00:03:43,840 --> 00:03:46,630
internal ducting that
that occurs inside the aircraft fan air

176
00:03:46,630 --> 00:03:46,640
that occurs inside the aircraft fan air
 

177
00:03:46,640 --> 00:03:47,830
that occurs inside the aircraft fan air
collection systems

178
00:03:47,830 --> 00:03:47,840
collection systems
 

179
00:03:47,840 --> 00:03:49,589
collection systems
valves and so on these things have to be

180
00:03:49,589 --> 00:03:49,599
valves and so on these things have to be
 

181
00:03:49,599 --> 00:03:51,910
valves and so on these things have to be
developed to make them compact

182
00:03:51,910 --> 00:03:51,920
developed to make them compact
 

183
00:03:51,920 --> 00:03:55,350
developed to make them compact
lightweight efficient yet at the same

184
00:03:55,350 --> 00:03:55,360
lightweight efficient yet at the same
 

185
00:03:55,360 --> 00:03:57,670
lightweight efficient yet at the same
time not have large pressure losses

186
00:03:57,670 --> 00:03:57,680
time not have large pressure losses
 

187
00:03:57,680 --> 00:04:00,390
time not have large pressure losses
at the 9 by 15 foot low speed wind

188
00:04:00,390 --> 00:04:00,400
at the 9 by 15 foot low speed wind
 

189
00:04:00,400 --> 00:04:00,869
at the 9 by 15 foot low speed wind
tunnel

190
00:04:00,869 --> 00:04:00,879
tunnel
 

191
00:04:00,879 --> 00:04:03,350
tunnel
at louis we are looking at some of the

192
00:04:03,350 --> 00:04:03,360
at louis we are looking at some of the
 

193
00:04:03,360 --> 00:04:05,030
at louis we are looking at some of the
problem areas

194
00:04:05,030 --> 00:04:05,040
problem areas
 

195
00:04:05,040 --> 00:04:08,390
problem areas
hot gas ingestion avoidance and ground

196
00:04:08,390 --> 00:04:08,400
hot gas ingestion avoidance and ground
 

197
00:04:08,400 --> 00:04:09,910
hot gas ingestion avoidance and ground
flow field effects

198
00:04:09,910 --> 00:04:09,920
flow field effects
 

199
00:04:09,920 --> 00:04:12,789
flow field effects
on stovall aircraft another technical

200
00:04:12,789 --> 00:04:12,799
on stovall aircraft another technical
 

201
00:04:12,799 --> 00:04:13,990
on stovall aircraft another technical
problem that we're looking at

202
00:04:13,990 --> 00:04:14,000
problem that we're looking at
 

203
00:04:14,000 --> 00:04:17,110
problem that we're looking at
is the hot gas ingestion problem

204
00:04:17,110 --> 00:04:17,120
is the hot gas ingestion problem
 

205
00:04:17,120 --> 00:04:18,789
is the hot gas ingestion problem
this is where while many of these

206
00:04:18,789 --> 00:04:18,799
this is where while many of these
 

207
00:04:18,799 --> 00:04:20,390
this is where while many of these
concepts have

208
00:04:20,390 --> 00:04:20,400
concepts have
 

209
00:04:20,400 --> 00:04:22,710
concepts have
hot gas which is produced forward on the

210
00:04:22,710 --> 00:04:22,720
hot gas which is produced forward on the
 

211
00:04:22,720 --> 00:04:25,430
hot gas which is produced forward on the
aircraft usually by burning fuel in

212
00:04:25,430 --> 00:04:25,440
aircraft usually by burning fuel in
 

213
00:04:25,440 --> 00:04:28,310
aircraft usually by burning fuel in
in the vertical lift system this hot gas

214
00:04:28,310 --> 00:04:28,320
in the vertical lift system this hot gas
 

215
00:04:28,320 --> 00:04:30,070
in the vertical lift system this hot gas
goes down hits the ground

216
00:04:30,070 --> 00:04:30,080
goes down hits the ground
 

217
00:04:30,080 --> 00:04:32,390
goes down hits the ground
is is reflected back up and ingested by

218
00:04:32,390 --> 00:04:32,400
is is reflected back up and ingested by
 

219
00:04:32,400 --> 00:04:34,790
is is reflected back up and ingested by
the inlet systems on the aircraft

220
00:04:34,790 --> 00:04:34,800
the inlet systems on the aircraft
 

221
00:04:34,800 --> 00:04:39,189
the inlet systems on the aircraft
and turbine engines do not like hot gas

222
00:04:39,189 --> 00:04:39,199
and turbine engines do not like hot gas
 

223
00:04:39,199 --> 00:04:41,270
and turbine engines do not like hot gas
they lose their power or they or

224
00:04:41,270 --> 00:04:41,280
they lose their power or they or
 

225
00:04:41,280 --> 00:04:42,629
they lose their power or they or
something else happens and

226
00:04:42,629 --> 00:04:42,639
something else happens and
 

227
00:04:42,639 --> 00:04:44,950
something else happens and
it's a major problem there are other

228
00:04:44,950 --> 00:04:44,960
it's a major problem there are other
 

229
00:04:44,960 --> 00:04:46,790
it's a major problem there are other
problems that are associated with

230
00:04:46,790 --> 00:04:46,800
problems that are associated with
 

231
00:04:46,800 --> 00:04:48,310
problems that are associated with
stovall aircraft

232
00:04:48,310 --> 00:04:48,320
stovall aircraft
 

233
00:04:48,320 --> 00:04:50,710
stovall aircraft
and in conjunction with nasa langley

234
00:04:50,710 --> 00:04:50,720
and in conjunction with nasa langley
 

235
00:04:50,720 --> 00:04:51,830
and in conjunction with nasa langley
research center

236
00:04:51,830 --> 00:04:51,840
research center
 

237
00:04:51,840 --> 00:04:54,950
research center
and nasa ames research center the nasa

238
00:04:54,950 --> 00:04:54,960
and nasa ames research center the nasa
 

239
00:04:54,960 --> 00:04:57,270
and nasa ames research center the nasa
lewis research center is continuing in

240
00:04:57,270 --> 00:04:57,280
lewis research center is continuing in
 

241
00:04:57,280 --> 00:04:58,230
lewis research center is continuing in
its quest

242
00:04:58,230 --> 00:04:58,240
its quest
 

243
00:04:58,240 --> 00:05:02,070
its quest
to produce a viable lightweight reliable

244
00:05:02,070 --> 00:05:02,080
to produce a viable lightweight reliable
 

245
00:05:02,080 --> 00:05:04,469
to produce a viable lightweight reliable
propulsion system these aircraft have to

246
00:05:04,469 --> 00:05:04,479
propulsion system these aircraft have to
 

247
00:05:04,479 --> 00:05:06,790
propulsion system these aircraft have to
operate efficiently at supersonic speeds

248
00:05:06,790 --> 00:05:06,800
operate efficiently at supersonic speeds
 

249
00:05:06,800 --> 00:05:09,430
operate efficiently at supersonic speeds
as well as at very low speeds

250
00:05:09,430 --> 00:05:09,440
as well as at very low speeds
 

251
00:05:09,440 --> 00:05:12,390
as well as at very low speeds
with very high air flows and as a result

252
00:05:12,390 --> 00:05:12,400
with very high air flows and as a result
 

253
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with very high air flows and as a result
there's a problem of getting

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there's a problem of getting
 

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there's a problem of getting
inlets that have high performance both

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00:05:16,150 --> 00:05:16,160
inlets that have high performance both
 

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00:05:16,160 --> 00:05:18,390
inlets that have high performance both
at supersonic conditions and also at

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at supersonic conditions and also at
 

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00:05:18,400 --> 00:05:20,790
at supersonic conditions and also at
essentially static conditions while in

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essentially static conditions while in
 

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essentially static conditions while in
hover

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hover
 

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hover
possibly at high angles of attack which

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00:05:23,909 --> 00:05:23,919
possibly at high angles of attack which
 

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possibly at high angles of attack which
which result in

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which result in
 

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which result in
in flow problems for the inlet system

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in flow problems for the inlet system
 

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in flow problems for the inlet system
nozzle systems are a key problem here

270
00:05:32,790 --> 00:05:32,800
nozzle systems are a key problem here
 

271
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nozzle systems are a key problem here
from the

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from the
 

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from the
standpoint that they tend to be in

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standpoint that they tend to be in
 

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standpoint that they tend to be in
today's aircraft very heavy if we

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today's aircraft very heavy if we
 

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today's aircraft very heavy if we
put the kind of requirements that a

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put the kind of requirements that a
 

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put the kind of requirements that a
stovall has so

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stovall has so
 

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stovall has so
so a major program has to be evolved to

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so a major program has to be evolved to
 

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so a major program has to be evolved to
develop advanced

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develop advanced
 

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develop advanced
nozzle concepts and last but not least

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00:05:47,830 --> 00:05:47,840
nozzle concepts and last but not least
 

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00:05:47,840 --> 00:05:48,950
nozzle concepts and last but not least
is the

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is the
 

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00:05:48,960 --> 00:05:50,790
is the
is the main is a key problem for the

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is the main is a key problem for the
 

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is the main is a key problem for the
pilot and that is

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pilot and that is
 

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pilot and that is
the pilot has to be able to control this

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the pilot has to be able to control this
 

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the pilot has to be able to control this
beast while he's

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beast while he's
 

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beast while he's
uh doing his mission and

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00:05:58,950 --> 00:05:58,960
uh doing his mission and
 

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00:05:58,960 --> 00:06:01,430
uh doing his mission and
the harrier is a difficult aircraft to

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the harrier is a difficult aircraft to
 

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the harrier is a difficult aircraft to
fly

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00:06:03,990 --> 00:06:04,000

 

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00:06:04,000 --> 00:06:05,749

one of the areas that we in conjunction

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one of the areas that we in conjunction
 

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one of the areas that we in conjunction
with aims we have a joint program with

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00:06:07,430 --> 00:06:07,440
with aims we have a joint program with
 

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00:06:07,440 --> 00:06:09,590
with aims we have a joint program with
aim specifically in this area

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00:06:09,590 --> 00:06:09,600
aim specifically in this area
 

309
00:06:09,600 --> 00:06:12,390
aim specifically in this area
to address how do we get the right pilot

310
00:06:12,390 --> 00:06:12,400
to address how do we get the right pilot
 

311
00:06:12,400 --> 00:06:13,350
to address how do we get the right pilot
interfaces

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00:06:13,350 --> 00:06:13,360
interfaces
 

313
00:06:13,360 --> 00:06:16,150
interfaces
there to fly the airplane in a manner

314
00:06:16,150 --> 00:06:16,160
there to fly the airplane in a manner
 

315
00:06:16,160 --> 00:06:16,629
there to fly the airplane in a manner
which

316
00:06:16,629 --> 00:06:16,639
which
 

317
00:06:16,639 --> 00:06:19,110
which
which makes it easy for him to fly we

318
00:06:19,110 --> 00:06:19,120
which makes it easy for him to fly we
 

319
00:06:19,120 --> 00:06:21,510
which makes it easy for him to fly we
could build a stovall airplane today

320
00:06:21,510 --> 00:06:21,520
could build a stovall airplane today
 

321
00:06:21,520 --> 00:06:23,189
could build a stovall airplane today
the problem is that it would be too

322
00:06:23,189 --> 00:06:23,199
the problem is that it would be too
 

323
00:06:23,199 --> 00:06:25,590
the problem is that it would be too
heavy and not particularly practical

324
00:06:25,590 --> 00:06:25,600
heavy and not particularly practical
 

325
00:06:25,600 --> 00:06:28,150
heavy and not particularly practical
for what it can do for a mission okay

326
00:06:28,150 --> 00:06:28,160
for what it can do for a mission okay
 

327
00:06:28,160 --> 00:06:28,629
for what it can do for a mission okay
and

328
00:06:28,629 --> 00:06:28,639
and
 

329
00:06:28,639 --> 00:06:30,469
and
the main thing that we're trying to

330
00:06:30,469 --> 00:06:30,479
the main thing that we're trying to
 

331
00:06:30,479 --> 00:06:31,830
the main thing that we're trying to
develop now

332
00:06:31,830 --> 00:06:31,840
develop now
 

333
00:06:31,840 --> 00:06:35,350
develop now
is a supersonic capability an aircraft

334
00:06:35,350 --> 00:06:35,360
is a supersonic capability an aircraft
 

335
00:06:35,360 --> 00:06:35,670
is a supersonic capability an aircraft
with

336
00:06:35,670 --> 00:06:35,680
with
 

337
00:06:35,680 --> 00:06:38,870
with
adequate range and reasonable payload

338
00:06:38,870 --> 00:06:38,880
adequate range and reasonable payload
 

339
00:06:38,880 --> 00:06:41,270
adequate range and reasonable payload
and that that's the main thrust of of

340
00:06:41,270 --> 00:06:41,280
and that that's the main thrust of of
 

341
00:06:41,280 --> 00:06:43,510
and that that's the main thrust of of
the advanced technology

342
00:06:43,510 --> 00:06:43,520
the advanced technology
 

343
00:06:43,520 --> 00:06:45,909
the advanced technology
we know that stovall works it's a

344
00:06:45,909 --> 00:06:45,919
we know that stovall works it's a
 

345
00:06:45,919 --> 00:06:47,909
we know that stovall works it's a
question of getting an aircraft which

346
00:06:47,909 --> 00:06:47,919
question of getting an aircraft which
 

347
00:06:47,919 --> 00:06:49,510
question of getting an aircraft which
provides the

348
00:06:49,510 --> 00:06:49,520
provides the
 

349
00:06:49,520 --> 00:06:51,189
provides the
or meets the requirements that the

350
00:06:51,189 --> 00:06:51,199
or meets the requirements that the
 

351
00:06:51,199 --> 00:07:00,639
or meets the requirements that the
services want