Attachment N-TAM_Table_R.pdf

Zones Legend

Q u a li fi c a ti o n

S ta tu s

S in e V ib ra ti o n D e fi n it io n

S tr u c tu ra l L o a d s

A c c e le ra ti o n

A c o u s ti c s

R a n d o m

V ib ra ti o n

S in e V ib ra ti o n

P y ro te c h n ic

S h o c k

T o rq u e o r

F o rc e

M a rg in

P re s s u re

P ro fi le

T h e rm a l

V a c u u m

T h e rm a l

B a la n c e

R F

A ir li n k

C o m p a ti b il it y

T e s t

C o n d u c te d

E m is s io n s

D if f

M o d e

C

E

C

E

C o n d u c te d

E m is s io n s

C o m m o n M o d e N o is e

C E

C

E

(3

C o n d u c te d

S u s c e p t.

P o w e r

L e a d s

C S

C o n d u c te d

S u s c e p t.

P o w e r

L e a d s

C S

C o n d u c te d

E m is s io n s

In s tr u m e n t O p V o lt

R ip p le

R a d ia te d

E m is s io n s

R E

E le c t

F ie ld s

R a d ia te d

S u s c e p ti b il it y

R

S

G ro u n d in g

I s o la ti o n

D e e p

D ie le c tr ic C h a rg in g

E le c tr o s ta ti c A rc

D is c h a rg e

E x te rn a l

S u rf a c e

-t o

-S u rf a c e

D ir e c t

D is c h a rg e

T

ID

D is p la c e m e n t

D a m a g e

S in g le

E v e n t E ff e c ts

S

E E

O th e r

(s e e

N o te s

KEY

* = See Note Column

A = Perform Analysis

Q = Perform Qualification Test

QHS = Qualification by Similarity (1)

PF = Perform Protoflight Test

FA = Perform Flight Acceptance Test

T = Perform Test at this Level of Assembly

- = Not Required

S = Verify at Flight System Level of Assembly

L = Verify at Higher Level of Assembly

A,T = Test if indicated by Analysis

E = Qualification by EEE Parts Plan, Confirm to show bounded env

"/" = "or", "&" = "and"

GeoI1

GeoI2

GeoS1

GeoI3

GeoS2

GeoI4

C&DH Subsystem GeoI1

C&DH Subsystem GeoI2 - GeoI4

C&DH Subsystem GeoS1

C&DH Subsystem GeoS2

Unit / Component level ..

Harness Subsystem GeoI1

Harness Subsystem GeoI2 - GeoI4

Harness Subsystem GeoS1

Harness Subsystem GeoS2

Unit / Component level ..

Electrical Power Subsystem GeoI1

Electrical Power Subsystem GeoI2 - GeoI4

Electrical Power Subsystem GeoS1

Electrical Power Subsystem GeoS2

Unit / Component level ..

Telecom Subsystem GeoI1

Telecom Subsystem GeoI2 - GeoI4

Telecom Subsystem GeoS1

Telecom Subsystem GeoS2

Unit / Component level ..

Guidance, Navigation, & Control GeoI1

Guidance, Navigation, & Control GeoI2 - GeoI4

Guidance, Navigation, & Control GeoS1

Guidance, Navigation, & Control GeoS2

Star Tracker Assembly (STA)

Reaction Wheel Assembly (RWA)

Inertial Measurement Unit ( MU)

Unit / Component level ..

Structures & Mechanisms GeoI1

Structures & Mechanisms GeoI2 - GeoI4

Structures & Mechanisms GeoS1

Radiation

GeoXO Flight System Element

Environmental Verification Program

Dynamics Thermal EMC

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Structures & Mechanisms GeoS2

Spacecraft Primary Structure (including Fasteners)

Solar Array Separation

Solar Array Gimbal

Unit / Component level ..

Thermal Control Subsystem GeoI1

Thermal Control Subsystem GeoI2 - GeoI4

Thermal Control Subsystem GeoS1

Thermal Control Subsystem GeoS2

Temperature Sensors (AD590)

Temperature Sensors (PRTD)

MLI, All-Kapton Layup

Unit / Component level ..

Propulsion Subsystem GeoI1

Propulsion Subsystem GeoI2 - GeoI4

Propulsion Subsystem GeoS1

Propulsion Subsystem GeoS2

Propellant Tank

Unit / Component level ..

Notes:

(1) For Qualification by Similarity, GeoXO levels and ranges apply and testing is required where previous qualification does not envelope requirements. Qualification by Similarity verification must be approved in advance by the Government.

(2) Test shall be run in agreement with the levels specified in the GIRD

(3) For the Spacecraft subsystems, requirements for the Conducted Emissions (CE101 & CE03) shall be derived.

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