LAUNCH COUNTDOWN SCRIPT

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The countdown officially begins at T-4:30 from the stated opening of the launch window stated in Section 1110 of this OSD.  At the opening of the countdown, it is assumed the vehicle and payload are staged on the launcher and the Pad/Blockhouse Voltage/Amp (V/A) checks are complete.
 

Shaded portions of the program time column of this countdown indicate these times are practice items conducted during the vertical payload checks

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9000    COUNTDOWN PROCEDURES

  9100    NASA ROLES AND RESPONSIBILITIES

The following definitions describe the roles and responsibilities of key NASA personnel:

Test Director (TD):        The WFF TD has authority over all operations conducted on the WFF Test Range.  The TD is responsible for assuring that all range policy, criteria, and external agreements are satisfied during the operations.  The TD is the only person with authority to resume the countdown after a “HOLD” has been declared.

Mission Manager (MM):  The designated WFF MM is responsible for the planning, coordinating and directing of operational support for assigned projects conducted at the WFF Test Range.  The MM is the author of the Operations and Safety Directive (OSD), which is designed to accomplish project objectives while complying with established policy, criteria, and procedures.  The MM is responsible for coordinating and directing project activities as necessary during the countdown.  The MM will apprise the TD and RSO of project status details and likewise keep the project personnel properly informed of range operational status.  The MM also serves as Assistant TD.

Range Safety Officer (RSO):  The WFF RSO is responsible for assuring the WFF safety policy, criteria, and procedures are not violated during operations, and to assure that risks are understood and are within acceptable limits.  The RSO has authority to stop work, or hold a launch if necessary.  The RSO will keep the TD and MM apprised of safety status, which could affect launch operations.

Launch Pad Supervisor (LPS):  The WFF or NSROC LPS is responsible for implementing operational procedures in the launch area in accordance with the project OSD.  The LPS or his designated representative must be present and shall monitor all procedures involving hazardous operations.  No hazardous procedures will be initiated without the LPS’s knowledge and consent.

Operations Safety Supervisor (OSS):  The WFF OSS has authority over all hazardous operations performed during preparation and launch activities.  The OSS or a designated OSS representative must be present and shall monitor all procedures involving hazardous operations.  No hazardous procedures will be initiated without his knowledge and consent.       

Payload Manager:  The Payload Manager will keep the MM apprised of program status.  The PM is responsible for assuring that programmatic objectives are achieved.  The PM has authority, with the Test Director’s concurrence, to conduct tests of program systems in accordance with procedures.

9200    ABBREVIATIONS USED IN COUNTDOWN

COMP …………………………………Computer 

FOTO ………………………………….Photograher

LPS …………………………………….Launch Pad Supervisor

MM …………………………………….Mission Manager

PGMR …………………………….……Programmer

PI ……………………………………….Principal Investigator

PLC …………………………………….Payload Control

PM ……………………………………..Payload Manager

PTM ……………………………………Payload Telemetry

RC ……………………………………..Radar Coordinator

RD ……………………………………..Recovery Director

ROA ……………………………………Range Operations Assistant

RSO …………………………………….Range Safety Officer

SURV …………………………………..Surveillance

TD ………………………………………Test Director

TM Readout …………………………….Telemetry Readout Room

TM Receiving …………………………..Telemetry Receiving Room

WW ……………………………………..Wind Weighting

9300    LAUNCH COUNTDOWN

All items are to be announced complete on Channel 1 of the WFF intercom unless preceded by “N” for no response required.  Each item will be performed only after previous items have been checked complete unless directed otherwise by the Test Director or his designee.  Refer to page 9001 for the list of operator title abbreviations.

All supporting elements of the operations are expected to keep the RCC advised of their status throughout the countdown.  However, after the “T-5 minute station check” only personnel reporting countdown items or elements which affect the “GO/NO GO” criteria will report.  The elements are designated with an “asterisk” in the T-5 minute station check.  The countdown (program time) will be stopped remotely by the Test Director (TD), Mission Manager (MM), the Range Safety Officer (RSO), or the programmer on command by the TD if necessary.

This countdown officially begins at T-4:30 from the stated opening of the launch window stated in Section 1110 of this OSD.  At the opening of the countdown, it is assumed the vehicle and payload are staged on the launcher and pad/blockhouse voltage/amp (V/A) checks are complete.

Shaded portions of the program time column of this countdown indicate these times are practice items conducted during the vertical payload checks. 

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

04-30-00

1

WW

Launch corner reflector balloon and track to maximum altitude.

03-30-00

2

ROA

All personnel be advised that the following launch will be conducted under NRW-3570, Orion 30.053 NO, OSD countdown procedure Rev. 0, dated May 2002.  Please respond on Channel 1 on the intercom.

 

LPS – Launch Pad Supervisor

PGMR – Programmer

RC – Radar Coordinator

PI – Principal Investigator

COMP – Computer

PM – Payload Manager

WW – Wind Weighting

RSO – Range Safety Officer

MM – Mission Manager

TD – Test Director

 

3

ROA

Establish RF avoidance for Pad 2.

 

4

LPS

Arm vehicle and payload.

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

 

5

LPS

Verify that the following tasks are complete:

1.  Vehicle and payload completely assembled on Pad 2 ARC launcher.

2.  Umbilical rigged and connected.

3.  Volt/Amp checks completed.

4.  Batteries charged.

1.      All safety restraints installed.

2.      Set Pre-Launch Danger Area roadblocks.

3.      Initial arming of Orion motor/payload.

03-00-00

6

TD,RSO,RSM

Conduct HOLD button checks.

 

7

LPS

Remove shelter.

 

8

FOTO

Take horizontal pictures of Orion.

 

9

ROA

Release RF avoidance at Pad 2.

02-30-00

10

WW

Release and track corner reflector balloon to 50 k ft. altitude.

 

11

ROA

Reset clock to T-8 minutes for the horizontal payload checks.

00-08-00

12

PLC

1.  Switch payload systems to EXT PWR ON in the following order:

2.  TM EXT PWR ON.

3.  Record TM 1 measurements.

Voltage _______ volts,     28 volts

Current _______ amps,    1.2 amps

4.      TRANSPONDER ON.

5.      Record TM Bus current.

Actual _______ amps,   1.5 amps

6.      Sub-SEM experiments ON.

7.      Record Experiment Bus measurements.

Voltage _______ volts,    12 volts

Current _______ amps,      0 amps

 

00-07-30

13

TM READOUT

8.  Start chart recorders.

 

 

 

 

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

 

14

TM RCVING

9.  Start magnetic tapes.

00-07-00

15

PLC

10.  ARM payload CDI system, verify GSE data.

11.  Record the following battery voltages:

Actual       Nom.

TM Battery           ______V         32V

Exp Battery          ______ V        12V

CDI Battery #1     ______ V        32V

CDI Battery #2     ______ V        32V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

00-06-30

16

RC

12.  Interrogate Pad 2 transponder and verify good signal.

 

17

PTM

13.  Verify data in limits on GDP’s.

 

18

PTM

14.  Verify chart recorder channels are nominal.

 

19

PTM

15.  Screen print numeric displays from GDP.

00-06-00

20

TM RCVING

16.  Record transmitter parameters.

Actual           Nominal

        TM Sig Str    ______ dB    >30 dB C/N

        Deviation      ______ KHz   +280 KHz

00-03-00

21

PLC

17.  Switch TM, transponder and experiment to INTERNAL power and record battery voltages below:

Actual          Nominal

TM battery   _____ V           30 V

Exp battery  _____ V            12 V

00-02-30

22

TM RCVING

18.  Verify no change in signal strength or deviation.

 

23

RC

19.  Verify radar transponder is still good.

00-02-00

24

PTM

20.  Verify data in limits on GDP.

00-00-00

25

PLC

21.  SAFE CDI system.

 

26

PLC

22.  Switch experiment, transponder and TM to EXTERNAL power.

 

27

PLC

23.  Switch experiment, transponder and TM OFF.

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

 

28

TM RCVING

24.  Stop mag tapes.

 

29

TM READOUT

25.  Stop chart recorders.

 

30

PM

Verify horizontal payload checks complete.

 

31

ROA

Reset countdown clock to terminal count.

02-00-00

32

COMP

Conduct simulation using nominal trajectory

 

33

TD

Initial contact with FAA, VACAPES, NORAD and recovery vessel.

 

34

TD

Release surveillance aircraft for take-off.

01-30-00

35

WW

Relay wind weighted payload impact coordinates to RD.

 

36

RD

Relay wind weighted payload impact coordinates to recovery aircraft and ship crew.

`

37

LPS

Elevate launcher to nominal settings:

AZ = 140°         EL = 82°

01-15-00

38

WW

Commence 15 minute interval wind weighting chaff balloon release schedule.  Track to an altitude of 6000 feet.

 

39

ROA

Establish RF avoidance on Pad 2.

 

40

ROA

Provide test rocket launcher setting.

 

41

LPS

Request permission from TD to load test rockets.

 

42

FOTO

Take vertical pictures and align Pad 2 cameras.

01-00-00

43

SURV

Surveillance aircraft on station with first ship report.

 

44

LPS

Clear launch danger area and set roadblocks.

 

45

LPS

Perform no voltage checks and connect firing circuits for test rockets.

 

46

LPS

Verify test rocket launcher danger area clear.

 

47

ROA

Release RF avoidance on Pad 2.

 

48

ROA

Reset clock to T-10 minutes for the vertical payload checks.

 

49

PM

Request permission to begin vertical checks.

 

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

00-08-00

50

PLC

1.  Switch payload systems to EXT PWR ON in the following order:

2.  TM EXT PWR ON.

3.  Record TM 1 measurements.

Voltage _______ volts,     28 volts

Current _______ amps,    1.2 amps

4.       TRANSPONDER ON.

5.      Record TM Bus current.

Actual _______ amps,   1.5 amps

6.      Sub-SEM experiments ON.

7.      Record Experiment Bus measurements.

Voltage _______ volts,    12 volts

Current _______ amps,      0 amps

 

00-07-30

51

TM READOUT

8.  Start chart recorders.

 

52

TM RCVING

9.  Start magnetic tapes.

00-07-00

53

PLC

10.  ARM payload CDI system, verify GSE data.

11.  Record the following battery voltages:

Actual       Nom.

TM Battery           ______V         32V

Exp Battery          ______ V        12V

CDI Battery #1     ______ V        32V

CDI Battery #2     ______ V        32V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

00-06-30

54

RC

12.  Interrogate Pad 2 transponder and verify good signal.

 

55

PTM

13.  Verify data in limits on GDP’s.

 

56

PTM

14.  Verify chart recorder channels are nominal.

 

57

PTM

15.  Screen print numeric displays from GDP.

 

 

 

 

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

00-06-00

58

TM RCVING

16.  Record transmitter parameters.

Actual           Nominal

        TM Sig Str    ______ dB    >30 dB C/N

        Deviation      ______ KHz   +280 KHz

00-03-00

59

PLC

17.  Switch TM, transponder and experiment to INTERNAL power and record battery voltages below:

Actual          Nominal

TM battery   _____ V           30 V

Exp battery  _____ V            12 V

00-02-30

60

TM RCVING

18.  Verify no change in signal strength or deviation.

 

61

RC

19.  Verify radar transponder is still good.

00-02-00

62

PTM

20.  Verify data in limits on GDP.

00-00-00

63

PLC

21.  SAFE CDI system.

 

64

PLC

22.  Switch experiment, transponder and TM to EXTERNAL power.

 

65

PLC

23.  Switch experiment, transponder and TM OFF.

 

66

TM RCVING

24.  Stop mag tapes.

 

67

TM READOUT

25.  Stop chart recorders.

 

68

PM

26.  Verify vertical payload checks are complete.

 

69

ROA

Reset countdown clock to terminal count.

00-30-00

70

TD

Inform Coast Guard of impending test rocket launches.

 

71

ROA

Launch test rockets.

00-20-00

72

TD

Clear recovery aircraft for take-off.

00-15-00

73

WW

Provide wind weighted launcher setting coordinates (degrees-min-sec) to RD.

 

74

ROA

Set launcher settings as specified by Range Safety Officer.

00-10-00

75

PGMR

Program HOLD is required.

 

76

RD

Verify recovery ship is on station.

 

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

00-09-00

77

ROA

Announce “This is NRW-3570 Sub-SEM Orion 30.053 NO launching from Pad 2, MRL launcher.  Please stand by for station checks.  All stations announce status as GO or NO GO on Channel 1.

 

*LPS

*PGMR

*RC (minimum of 2 C-band radars)

*TM (minimum of 2 antennas)

*Computer (RTCS and RTBS)

*RD (Recovery boat on station; sea state less than

                 4 feet)

*PI

*PM

CAM5

CAM15

Sounding Rocket Program Office Representative

*Mission Manager

*RSO (Ceiling minimums at both launch and

                   recovery sites; surface winds; launch

                   hazard area clear; air/surface hazard

                   area within limits)

*TD (R-6604, VACAPES, NORAD clearances)

 

78

TD

Test Director final briefing on “HOLD” procedures.

Announce “All stations are responsible for reviewing the GO/NO GO criteria listed in the OSD.  Only stations annotated with an asterisk are permitted to call a HOLD.  All other sites should report RED.”

00-08-00

79

PLC

1.  Switch payload systems to EXT PWR ON in the following order:

2.  TM EXT PWR ON.

3.  Record TM 1 measurements.

Voltage _______ volts,     28 volts

Current _______ amps,    1.2 amps

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

 

 

 

4.       TRANSPONDER ON.

5.      Record TM Bus current.

Actual _______ amps,   1.5 amps

6.      Sub-SEM experiments ON.

7.      Record Experiment Bus measurements.

Voltage _______ volts,    12 volts

Current _______ amps,      0 amps

 

00-07-30

80

TM READOUT

8.  Start chart recorders.

 

81

TM RCVING

9.  Start magnetic tapes.

00-07-00

82

PLC

10.  ARM payload CDI system, verify GSE data.

11.  Record the following battery voltages:

Actual       Nom.

TM Battery           ______V         32V

Exp Battery          ______ V        12V

CDI Battery #1     ______ V        32V

CDI Battery #2     ______ V        32V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

Capow Pac          ______ V        33V

00-06-30

83

RC

12.  Interrogate Pad 2 transponder and verify good signal.

 

84

PTM

13.  Verify data in limits on GDP’s.

 

85

PTM

14.  Verify chart recorder channels are nominal.

 

86

PTM

15.  Screen print numeric displays from GDP.

00-06-00

87

TM RCVING

16.  Record Transmitter parameters.

                              Actual             Nominal

       TM Sig Str     _____ dB        >30 dB C/N

       Deviation       _____ KHz      +280 KHz

00-05-00

88

PLC

17.  Switch SOIDAR Experiment ON.

 

“T” MINUS

HH-MM-SS

ITEM

ACT BY

OPERATION

 

89

PLC

18.  Record the following:

       SOIDAR Current ______ mA,   630 mA

00-03-00

90

PLC

19.  Switch TM, transponder and experiment to INTERNAL power and record battery voltages below:

                                      Actual           Nominal

       TM Battery            _____ V           30 V

       Exp Battery            _____ V           12 V

00-02-30

91

TM RCVING

20.  Verify no change in signal strength or deviation.

 

92

RC

21.  Verify radar transponder.

00-02-00

93

PTM

22.  Verify data in limits on GDP.

00-01-00

94

PLC

23.  Switch Glennbrook Systems ON and CONFIRM.

00-00-10

95

PGMR

Time count at one second intervals to T-0 thru T+10 seconds then every 10 seconds to T+1 minute.

00-00-08

96

PLC

24.  Switch SOLARE ON and CONFIRM.

00-00-00

97

 

Orion ignites (vehicle and payload umbilicals disengage).

 

 

 

 

 

 



“T” PLUS

HH-MM-SS

ITEM

ACT BY

OPERATION

00-00-32.5

98

 

Orion burnout.

00-01-25

99

 

Payload separation.

00-02-00.5

100

 

Apogee.

00-03-05

101

 

Orion ballistic impact.

00-03-33

102

 

Parachute deployment.

00-10-32

103

 

Payload/parachute impact.

 

104

TM RCVING

LOS.  Stop mag tapes.

 

105

TM READOUT

Stop chart recorders.

00-17-00

106

RD

Begin recovery operations.  Relay actual payload impact to recovery aircraft and recovery boat.

 

 

 

 

 

 

 

When operations in RCC are complete, release:

Electric shop (ext. 1446)

A/C shop (ext. 1511)

Generator room (ext. 2225)

 

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