hn gn i uete NASA Dryden FAA NY Office H Henwood Rod Bart ...€¦ · o f w e b p o r t a l lo (~ $...
46
Flight Test Hazard Planning Near the Speed of Light Bart Rod Henwood Huete NASA Dryden FAA NY Office https://ntrs.nasa.gov/search.jsp?R=20070021634 2020-07-17T20:27:18+00:00Z
Transcript of hn gn i uete NASA Dryden FAA NY Office H Henwood Rod Bart ...€¦ · o f w e b p o r t a l lo (~ $...
Flig
ht T
est H
azar
d P
lann
ing
Nea
r th
e Sp
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of L
ight
Bar
t
R
odH
enw
ood
H
uete
NA
SA
Dry
den
F
AA
NY
Offi
ce
https://ntrs.nasa.gov/search.jsp?R=20070021634 2020-07-17T20:27:18+00:00Z
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Onl
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Res
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rF
light
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t Sa
fety
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ewis
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iona
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t Sch
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bje
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rob
ab
ility
of
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urr
ence
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ate
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itle
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tall
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ract
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prob
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use
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s:
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Min
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ltit
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20
00
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AG
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5 4
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t A
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asy
mm
etri
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ow
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ult
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raft
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p a
pp
roac
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forw
ard
cg
bef
ore
aft
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p
ow
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ff b
efo
re p
ow
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n
iii.
win
gs
leve
l bef
or
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rnin
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1 k
t/se
c be
fore
acc
eler
ated
v.
term
inat
e bu
ildu
p if
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ank
ang
le li
mit
s ar
e ex
ceed
ed
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Do
no
t ad
d p
ow
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uri
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eco
very
unt
il ab
ove
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Vs
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Dep
artu
re/s
pin
rec
ove
ry d
iscu
ssed
in p
refl
ight
bri
efin
g.
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erg
ency
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ced
ure
s:
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If a
ircr
aft
dep
arts
co
ntro
lled
flig
ht, i
mm
edia
tely
ret
ard
po
wer
to id
le a
nd c
entr
aliz
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ntro
ls.
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If a
ircr
aft
ente
rs s
pin
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om
plis
h sp
in r
eco
very
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ced
ure
.
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k L
evel
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ter
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imiz
ing
pro
ced
ure
s ta
ken
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acc
ou
nt):
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igh
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ium
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w
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.
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ard
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se
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ect
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imiz
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sug
gest
ions
in e
ach
area
•R
emov
e du
plic
atio
n
•M
ake
the
data
base
eas
ier
to u
se
Exa
mpl
e M
atur
atio
n
Par
t 25
Sta
ll H
azar
ds
NTP
S20
Man
y V
arie
d In
puts
•Si
x di
ffer
ent
orga
niza
tion
s su
bmit
ted
inpu
ts f
or s
talls
•T
otal
of
66 d
iffe
rent
TH
A’s
–M
any
redu
ndan
t / n
earl
y th
e sa
me
•U
sed
19 d
iffe
rent
Haz
ard
Tit
les
•U
sed
14 d
iffe
rent
Man
euve
r N
ames
•A
ple
thor
a of
ver
bose
Haz
ards
iden
tifi
ed
•H
undr
eds
of m
itig
atio
ns–
Aga
in m
any
wer
e re
dund
ant
“Th
ere
is a
ris
k o
f st
all/d
epar
ture
fro
m c
on
tro
lled
flig
ht
wh
enin
crea
sin
g a
ng
le-o
f-at
tack
at
low
airs
pee
ds.
”
NTP
S21
Mat
ured
Sta
ll H
azar
ds
•In
the
end
, six
sta
ll ha
zard
s w
ere
iden
tifi
ed1.
Los
s of
con
trol
2.L
oss
of o
pera
ting
eng
ine(
s)
3.St
all/s
pin
chut
e fa
ils t
o de
ploy
4.St
all/s
pin
chut
e fa
ils t
o je
ttis
on w
hen
com
man
ded
5.R
ecov
ery
chut
e un
com
man
ded
depl
oym
ent
6.D
epar
ting
run
way
sur
face
(D
urin
g gr
ound
tes
t of
sta
ll sp
in c
hute
)
NTP
S22
Los
s of
Con
trol
Mit
igat
ions
•“L
oss
of C
ontr
ol”
mit
igat
ions
mat
ured
into
jus
t tw
elve
•T
he m
atur
ed m
itig
atio
ns in
clud
e:1.
Do
stal
l tes
ting
in a
bui
ldup
app
roac
h:
a.
fro
m le
ast
risk
to
high
est
risk
i. fo
rwar
d cg
, mid
cg,
aft
cg
ii. P
ower
off
bef
ore
pow
er o
n
iii. W
ings
leve
l bef
ore
turn
ing
iv. 1
kt/
sec
befo
re 3
kt/
sec
b.
ter
min
ate
build
up if
FA
R li
mit
s on
ban
k an
gle
are
exce
eded
at
any
poin
t of
the
bui
ldup
NTP
S23
Mit
igat
ions
(con
tinu
ed)
2. E
stab
lish
min
imum
alt
itud
es f
or:
a
. ent
ry,
b
. rec
over
y in
itia
tion
,
c
. rec
over
y ch
ute
depl
oym
ent
and
d
. man
ual b
ailo
ut.
3. P
erfo
rm p
re-f
light
che
cks
of s
tall
war
ning
and
sti
ck p
ushe
r, a
sap
plic
able
.
4. A
nti-
spin
chu
te m
ust
be in
stal
led,
fun
ctio
nal a
nd a
rmed
. P
erfo
rmpr
e-fl
ight
and
pre
-man
euve
r ch
ecks
of
chut
e as
app
licab
le.
5. M
inim
um c
rew
onb
oard
.
6. E
mer
genc
y E
gres
s sy
stem
mus
t be
inst
alle
d an
d ar
med
. P
erfo
rmpr
e-fl
ight
and
pre
-man
euve
r ch
ecks
of
egre
ss s
yste
m a
s ap
plic
able
.
NTP
S24
Mit
igat
ions
(con
tinu
ed)
7. C
rew
to
wea
r he
lmet
s an
d pa
rach
utes
.
8. S
urfa
ce w
inds
mus
t be
less
tha
n xx
kts
(pa
rach
ute
depe
nden
t).
9. N
o ag
grav
ated
inpu
t st
alls
. All
stal
ls w
ill b
e ba
llce
nter
ed.
10. N
o as
ymm
etri
c po
wer
sta
lls.
11. I
f de
part
ing
cont
rolle
d fl
ight
ret
ard
thro
ttle
s to
idle
and
cent
raliz
e co
ntro
ls.
12. D
o no
t ad
d po
wer
dur
ing
reco
very
unt
il ai
rspe
ed is
incr
easi
ng a
bove
1.2
Vs.
NTP
S25
Look
for
“Tes
t Haz
ard
Dat
abas
e”
Info
rmat
ion
Avi
atio
n Li
nks
1
2 3
NTP
S26
FA
A A
cces
s
NTP
S27
FA
A A
cces
s
NTP
S28
FA
A A
cces
s
NTP
S29
NA
SA P
BM
A W
ebsi
te L
ink
http
://pb
ma.
nasa
.gov
/ftsd
b/ho
me.
aspx
NTP
S30
http
://p
bma.
nasa
.gov
/ftsd
b/
NTP
S31
NTP
S32
NTP
S33
FA
R R
efer
ence
Sea
rch
NTP
S34
Rec
ord
Fie
ld S
earc
h
NTP
S35
NTP
S36
1
2
3
Key
wor
d Se
arch
NTP
S37
Res
ults
of
FA
R R
efer
ence
Sea
rch
NTP
S38
Haz
ard
s Cau
ses
Mit
igat
ion
s
Tes
tD
etai
ls
NTP
S39
NTP
S40
In C
oncl
usio
n
•T
he m
atur
ed T
HA
dat
abas
e IS
a w
ide
arra
y of
tes
tsa
fety
idea
s an
d su
gges
tion
s–
But
it is
NO
T a
n F
AA
-man
date
d so
luti
on
–It
is N
OT
a g
over
nmen
t-ap
prov
ed s
olut
ion
–A
nd it
is N
OT
an
auto
-saf
ety
plan
ning
dev
ice
•T
he m
atur
ed h
azar
ds, c
ause
s an
d m
itig
atio
ns a
re n
eces
sari
lyge
neri
c
•Y
our
test
will
hav
e un
ique
pro
blem
s an
d w
ill r
equi
re u
niqu
eso
luti
ons
•T
he T
HA
dat
abas
e ca
n be
an
exce
llent
sta
rtin
g po
int
Fed
eral
Avi
atio
nA
dm
inis
trat
ion
41F
TS
Dat
abas
e U
pd
ate
May
. 200
7
In C
on
clu
sio
n
•M
ilita
ry/R
esea
rch
Dat
abas
e S
tatu
s–
Dat
a un
der
deve
lopm
ent
at m
onth
ly W
ebex
/tele
con
mee
tings
•C
on
tact
Jo
e O
rwat
(x38
66)
or
Bar
tH
enw
oo
d (
x574
6)A
t N
AS
A D
ryd
en (
661)
276-
xxxx
Bri
anM
arko
wic
h(N
AV
AIR
Pax
Riv
er)
4th Th
urs
day
at 0
900
PS
T
Pro
pu
lsio
n
Kim
Han
ks(A
rmy
Tes
t&
Tra
inin
gC
ente
r)
1st Th
urs
day
at 0
900
PS
T
Ro
tary
Win
g Ic
ing
Ku
rtB
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ken
shi
p (
Gle
nR
esea
rch
Cen
ter)
3rd Wed
nes
day
at 0
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PS
T
Fix
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me
Tes
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Pro
puls
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Pro
puls
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Kim
Han
ks (
Arm
y T
est &
Kim
Han
ks (
Arm
y T
est &
Tra
inin
g C
ente
r)T
rain
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Cen
ter)
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hurs
day
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hurs
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imD
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itiat
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ht te
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mis
sion
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t/Dat
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ubm
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odul
e
ννC
reat
e re
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nce
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rmat
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Cre
ate
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renc
e in
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atio
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irwor
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t saf
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revi
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roce
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