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时间:2010-05-30 09:34来源:蓝天飞行翻译 作者:admin
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S T P S ta n d a rd Te m pera t u re and Press u re
S T S S ta ble Ti me Subfie ld
S T X S ta rt of Text
S U S ignal Un i t
S UA S pec ial Use Ai r s pace
S U L Yaw Da m per Act u a tor
S U O ( 1 ) Ai leron / Eleva tor / R u d d er Servo
( 2 ) Servo Act u a tor
S u p e r - A rece iver in wh ich the inc om i ng RF sign a l
h e t e r o d y n e is mixed to produce a lower intermedia te
Re c e i v e r freque nc y.
S u p p r e s s o r A p ul se used to di sa ble L-band avion ics du ri ng th e
P u l s e tra n s m i t t i ng period of anoth er piece of L-ba n d
a i r borne equi pme n t . It preve n ts the oth er avion ic s
a boa rd the airc raft from be i ng damaged or interfered
wi th by the tra n s m i ss ion and any noi se assoc ia ted
wi th that tra n s m i ss ion .
S U P P S Regional Supple me n ta ry Procedu res
S U T ( 1 ) Au to th ro t tle Servo
( 2 ) S ta bi l izer Trim Servo
( 3 ) System Un d er Test
S V S pace Ve h ic le
S V C ( 1 ) Service
( 2 ) Swi tch ed Vi rtual Circui t
S VO Servo
S V R R Service Rea di n ess Review
S V T Servo T h ro t tle
S S U S u bsequent Signal Un i t
S T S ta t i st ic s
s t a S ta t ion
S TA B S ta bi l izer
S t a n d a r d Re prese n ts the mean or average pro pert ies of th e
A t m o s p h e r e a tm os p h ere. At sea level sta t ic press u re is 29.92 In H g
and te m pera t u re is +15 ° C.
S t a n d b y A DME mode that appl ies power to the DME RT b u t
M o d e the unit does not tra n s m i t .
S TA R S ta n d a rd Terminal Arrival Ro u tes
S TA R S S ta n d a rd Terminal Au tom a t ion Re place ment Syste m
Static Po r t s Fl us h - m o un ted ope n i ngs in the skin of the airc raft
fuse lage used to se n se sta t ic press u re.
S t a t i c Am bient atm os p h eric press u re or sta t ic press u re is
P r e s s u r e the force per unit area exerted by the air on th e
s u rface of a body at rest re la t ive to the air.
Static RAM RAM con structed of bi sta ble tra n s i stor ele me n ts.
Me m ory cells do not requi re refres h i ng.
( See Dyn a m ic RA M.)
Static Source Ac orrect ion appl ied to sta t ic so u rce press u re
Error (SSEC) mea s u re me n ts to pa rtly or com ple te ly correct for
press u re errors that are caused by airflow ch a nges. It is
c om p u ted as a funct ion of Mach and altitude ba sed on
mea s u red errors for a pa rt icular sta t ic syste m .
S T B Systems Test bed
S T B Y S ta n dby In strume n ts
S TC ( 1 ) Se n s i t ivi ty Ti me Con trol .A c on trol circuit used
in radar appl ic a t ions to con trol rece iver gain wi th
res pect to time.
( 2 ) S u p ple me n tal Type Cert i fic a te
S TC M S ta bi l izer Trim Con trol Module
S T D ( 1 ) S ta n d a rd
( 2 ) System Tech n ical Desc ri p t ion
S T D B Y S ta n dby In strume n ts
9 4
9 7
TAU TAU is the minimum time a fl ight crew needs to
di scern a col l i s ion th reat and take eva s ive act ion . It
re prese n ts the perform a nce enve lo pe (speed and pa th
of airc raft) divid ed by the clos u re ra te of any intru d er
a i rc raft (TCA S ).
TAW S Terrain Awa re n ess Wa rn i ng Syste m
T B B Tra n sfer Bus Breaker
T B D To Be De term i n ed
T B O Ti me Be tween Overh aul s
T B S ( 1 ) To Be Spec i fied
( 2 ) To Be Suppl ied
TC ( 1 ) Tra n s port Con n ect ion
( 2 ) Type Cert i fic a te
T / C To p - of - C l i m b
TCA ( 1 ) Terminal Con trol Area
( 2 ) T h ro t tle Con trol Asse m bly
TCA S Traffic A lert Col l i s ion Avoid a nce Syste m
TCAS I A ba seline system that provid es a wa rn i ng (TA) to th e
fl ight crew of the prese nce of anoth er airc raft
( po te n t ial col l i s ion th reat) wi thin the surve i l la nce
a rea . No avoid a nce maneuver is sug gested.
TCAS II A c ol l i s ion avoid a nce system providi ng traffic
i nform a t ion (wi thin approxi m a te ly 30 nmi of th e
a i rc raft) to the fl ight crew, in addi t ion to the resol u t ion
a dvi sories (RA) (for vert ical maneuvers only ). A
TCA S I I - equi p ped airc raft will coordi n a te wi th
TCA S I I - equi p ped intru d er airc raft to provid e
c om ple me n ta ry maneuver s.
TC C Tu r bine Case Cool i ng
TC F Terrain Clea ra nce Floor
TC M Tech n ical Coordi n a t ion Mee t i ng
TC M S Test Con tent Ma n age ment Syste m
TC N TACA N
TC P Tra n s m i ss ion Con trol Pro toc ol
S V U Sa te l l i te Voice Un i t
S / W Softwa re
S WA P Severe Wea th er Avoid a nce Progra m
S W I T Softwa re In tegra t ion and Test
S W T R R Softwa re Test Rea di n ess Review
 
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