5.0 MISSION IMPLEMENTATION

Mission implementation is primarily concerned with DC-8 and P-3B aircraft operations. Additionally, there is the operation of the C-130 cargo plane, ozonesonde network measurements, meteorological support measurements, ground station measurements, and satellite data products. The ground station measurements will be conducted by two PI’s (see Section 4.5) to obtain vertical column amounts of selected trace gas species and supplementary ozonesondes. The mission deployment schedule is given in Table 5.0-1.

5.1 DC-8 and P-3B Operations

The nominal flight schedule for the DC-8 and P-3B aircraft are given in Table 5.0-1 and the nominal flight tracks are shown in Figure 2.4-1 and Figure 2.4-2. Nominal flight profiles are shown in Appendix D. Layout of the instruments aboard each aircraft is shown in Figures 4.2. Aircraft characteristics are listed in Appendix C.

Measurement systems installation and integration aboard the DC-8 will be performed at the NASA Dryden Flight Research Center where systems checkout flights will also be conducted. The same functions will be performed at the NASA Wallops Flight Center for the P-3B. Both aircraft will begin the deployment for TRACE-P with a transit flight from the U.S. West Coast to Kona, Hawaii. The two aircraft will proceed to Hong Kong and then to Yokota AFB, Japan where they will conduct coordinated local flights – 5 each at Hong Kong and Yokota.  The P-3B will then transit to Midway Island where one local flight will be conducted.  The DC-8 will transit from Yokota to Kona, Hawaii and conduct one local flight at Kona.  Following the Midway Island flight the P-3B will transit to Kona.  Both planes will return to their home bases of Dryden and Wallops, respectively.    

5.2 C-130 Operations

The Wallops C-130 will transport critical cargo and expendables unable to be pre-shipped or carried on the DC-8 or P-3B. It will also provide for supplementary P-3B crew. The C-130 will initially load P-3B related items at Wallops and then proceed with the P-3B to Dryden where it will load DC-8 related items. The C-130 will accompany the P-3B to Hong Kong, Japan, and back to Wallops. The DC-8 will have the same flight itinerary whenever possible.

Table 5.0-1   P-3B, DC-8, and C-130 Nominal Schedule During TRACE-P

Date

P-3B

Best Time

Flt. Hrs. Alloc.

DC-8

Best Time

Flt. Hrs. Alloc.

C-130

Best Time

Flt. Hrs. Alloc.

WDL

EDL

 

11 Dec

Begin install inlets and plumbing

               

 

02
Jan

 

 

 

Begin install inlets and plumbing 

 

 

 

 

 

 

08
Jan

Racks avail. to begin installation

 

 

Racks avail. to begin installation

 

 

 

 

 

 

15
Jan

Holiday

 

 

Holiday

 

 

Holiday

 

 

 

23 Jan

      CCB Hazard Review          

 

25
Jan

 

 

 

Complete Rack  Install and C/O.

 

 

 

 

 

 

26 Jan

Complete Rack Install and C/O

               

 

29
Jan

Wallops

 

 

Tech Brief

 

 

 

 

 

 

30
Jan

Wallops

 

 

Cmplt. Elect/DADS & Power Ck

 

 

 

 

 

 

31
Jan

Wallops

 

 

Rollout, Wt. & Balance, etc

 

 

 

 

 

 

01
Feb

Wallops

 

 

Engineering Check & ICATS Flight

 

2

 

 

 

 

02
Feb

Wallops

 

 

Pilot Proficiency Flight

 

 

 

 

 

 

03
Feb

Wallops

 

 

Laser Calibrations

 

 

 

 

 

 

04
Feb

Wallops

 

 

Laser Calibrations

 

 

 

 

 

 

05
Feb

Wallops

 

 

ICATS RVSM cert. Flight

 

 

 

 

 

 

06
Feb

Complete power check and hazard analysis

 

2

Laser Calibrations

 

 

 

 

 

 

07
Feb

Safety brief and FRR

 

 

Laser Calibrations

 

 

 

 

 

 

08
Feb

Engineering Check Flight

 

2

Laser Calibrations

 

 

 

 

 

 

09
Feb

Test Flight 1

 

2.5

Laser Calibrations

 

 

 

 

 

 

10
Feb

Wallops

 

 

Laser Calibrations

 

 

 

 

 

 

11
Feb

Wallops

 

 

Dryden

 

 

 

 

 

 

12
Feb

Test Flight 2

 

3.5

Mandatory Safety Briefing

 

 

 

 

 

 

13
Feb

Wallops

 

 

Dryden

 

 

 

 

 

 

14
Feb

Wallops

 

 

Test Flight 1

 

3

 

 

 

 

15
Feb

Test Flight 3

 

5.5

ORR

 

 

 

 

 

 

16
Feb

C-130 load ready in N-159

  

 

Test Flight 2

  

  

  

  

 

17
Feb

Wallops

 

 

Dryden

 

 

 

 

 

 

18 Feb

Wallops

   

Dryden

          

 

19
Feb

Holiday--Wallops Pack

 

 

Holiday

 

 

Holiday

 

 

 

20
Feb

Wallops Pack & Load C-130

 

 

Test Flight 3

 

6

Upload P-3B Equipment

 

 

  

21
Feb

Wallops Pack & Load C-130

 

 

Dryden Pack

  

 

Upload P-3B Equipment

  

  

 

22
Feb

Delay

 

 

Dryden Pack

   

   

Delay

 

 

 

23
Feb

Delay

 

 

Dryden Pack & load C-130

 

 

Transit: Wallops to Dryden

7.9 

7.9 

 

24
Feb

Transit: Wallops to Palmdale

6.8

8.5

Dryden Pack

 

 

Transit: DFRC to Palmdale

0.4

0.4

 

25
Feb

Palmdale

 

 

Dryden Pack

 

 

Palmdale

 

 

27
Feb

26
Feb

Transit: Palmdale to Kona, Hawaii 

7.5

8.5

Transit: Dryden to Kona, Hawaii

5.9

8

Transit: Palmdale to Kona, Hawaii 

8.6

8.6

28
Feb

27
Feb

Transit: Kona, Hawaii to Wake Isl.

6.3

8.5

Transit: Kona, Hawaii to Guam

8.4

10

Transit: Kona, Hawaii to Wake Isl.

7.1

7.1

01
Mar

28
Feb

Wake Island

 

 

Guam

  

  

Wake Island

 

 

02
Mar

01
Mar

Transit: Wake Island to Guam

4.1

6

Guam

 

 

Transit: Wake Island to Guam

4.7

4.7

03
Mar

02
Mar

Guam

 

 

Guam

 

 

Guam

 

 

04
Mar

03
Mar

Transit: Guam to Hong Kong

6.1

8

Transit: Guam to Hong Kong

4.8

7

  Transit: Guam to Hong Kong

7.0

7.0

05
Mar

04 Mar

Hong Kong 

  

 

Hong Kong 

 

 

   Offload all equipment

   

06
Mar

05
Mar

Hong Kong Local 1

 

Hong Kong Local 1

10

 

  

 

 

07
Mar

06
Mar

Down Day

    

 

Down Day

  

 

    

   

   

08
Mar

07
Mar

Hong Kong 

  

8

Hong Kong 

 

8

  

  

  

09
Mar

08
Mar

Hong Kong Local 2 to Okinawa

2.7 

 8

Hong Kong Local 2 to Okinawa

2.1 

10 

 

 

 

10
Mar

09
Mar

Hong Kong Local 3 Okinawa to Hong Kong

 2.9

8

Hong Kong Local 3 Okinawa to Hong Kong

2.3 

 

 

 

11
Mar

10
Mar

Hong Kong

 

 

Hong Kong

 

 

 

 

 

12
Mar

11
Mar

Hong Kong 

 

 

Hong Kong 

 

 

 

 

 

13
Mar

12
Mar

Hong Kong Local 4

 

Hong Kong Local 4

 

 

 

 

14
Mar

13
Mar

Hong Kong 

  

  

Hong Kong 

  

  

 

  

  

15
Mar

14 Mar

Hong Kong Pack

 

 

Hong Kong Pack

  

  

  

 

 
16
Mar
15  Mar

Hong Kong Pack

  

  

Hong Kong Pack

   

  

Upload all equipment

  

  

17
Mar
16 Mar

Transit: Hong Kong to Okinawa

2.7 

8

Transit: Hong Kong to Okinawa

2.1 

9

Transit: Hong Kong to Okinawa

3.1 

 3.1

18
Mar

17 Mar

Transit: Okinawa to Yokota AB

2.7

8

Transit: Okinawa to Yokota AB

2.1

10

Transit: Okinawa to Yokota AB

3.1

3.1

19
Mar
18  Mar

Yokota AB

 

 

Yokota AB

 

 

 

 

 

20
Mar

19
Mar

Yokota AB

 

 

Yokota AB crew changeout

 

 

 

 

 

21
Mar

20  Mar

Yokota Local 1

 

8

Yokota Local 1

 

8

 

 

 

22
Mar

21
Mar

Down Day

 

 

Down Day

 

 

 

 

 

23
Mar

22
Mar

Yokota AB

 

 

Yokota AB

 

 

 

 

 

24
Mar

23
Mar

Yokota Local 2

 

8

Yokota Local 2

 

 8

 

 

 

25
Mar

24
Mar

Yokota AB

 

 

Yokota AB

 

 

 

 

 

26
Mar

25
Mar

Yokota AB

 

 

Yokota AB 

 

 

 

 

 

27
Mar

26
Mar

Yokota Local 3

 

 6

Yokota Local 3

 

 8

 

 

 

28
Mar

27
Mar

Yokota AB

 

 

Yokota AB

 

 

 

 

 

29
Mar

28
Mar

Yokota AB

  

 

Yokota AB

  

 

  

  

  

30
Mar

29
Mar

Yokota Local 4 Yokota to Okinawa

 3

Yokota Local 4 Yokota to Okinawa

 2.3

10 

 

 

 

31
Mar

30
Mar

Yokota  Local 5 Okinawa to Yokota

 2.7

Yokota  Local 5 Okinawa to Yokota

2.1 

 8

 

 

 

01
Apr

31
Mar

Down Day

 

 

Down Day

 

 

 

 

 

02
Apr

01 Apr

Yokota  Pack

  

 

Yokota  Pack

  

 

  Upload all P-3B Equipment

     

03
Apr

02
Apr

Yokota Pack

  

  

Yokota Pack

 

 

Upload all DC-8 Equipment

  

  

04
Apr

03
Apr

Transit: Yokota AB to Midway

5.5 

Transit: Yokota AB to Kona, Hawaii

8.5 

 10

Transit: Yokota AB to Midway

 6.2

 6.2

05
Apr

04
Apr

Midway

  

 

Kona

 

 

Midway

 

 

 

05
Apr

Midway Local 1

  

8

Kona Local 1

   

10

Midway

   

  

  

06
Apr

Midway Pack

  

  

Down Day

  

  

Midway

  

  

 

07
Apr

Transit: Midway to Kona, Hawaii

3.2

4

Kona Pack

 

 

Transit: Midway to Kona, Hawaii

3.6

3.6

 

08
Apr

Kona, Hawaii

 

 

Kona, Hawaii

 

 

Reload and Upload DC-8

 

 

   

09
Apr

Transit: Kona, Hawaii to Dryden

6.3 

6.5 

Transit: Kona, Hawaii to Dryden

5.3 

8

Transit: Kona, Hawaii to Dryden

 7.1 

7.1

 

10
Apr

Transit: Dryden to WFF

5.3

7

Off Load

 

 

Transit: Dryden to WFF

6

6

 

11
Apr

Off Load

  

  

Off Load

 

 

Off Load P-3B Equipment

   

  

  

12
Apr

Off Load

  

  

Off Load

  

  

Off Load P-3B Equipment

  

  

  

13
Apr

Off Load

  

  

Complete

  

  

Complete

  

  

 

14
Apr

Off Load

 

 

Complete

 

 

Complete

 

 

 

15 Apr

Complete

               
   

Total Flight Hours Planned

 

172.5

   

163

  64.8 64.8

   

  

Total Flight Hours Available

  

172.5

  

  

163

  

 

 

 

 

5.3 Ozonesonde Network Measurements

Supporting measurements for the TRACE-P mission include releases from Trinidad Head, California; Hilo, Hawaii; Sapporo, Tsukuba, Naha, and Kagoshima, Japan; Java, Indonesia; Fiji; American Samoa; Hong Kong; Taiwan; and Cheju Island, Korea (Figure 2.5-1). The sondes from Trinidad Head, California and Hilo Hawaii are included in TRACE-P as sites operated by PI Sam Oltmans (see section 4.5.2).  The Cheju Island, Korea site is operated by Jae Kim, a co-investigator of Sam Oltmans.  The Sapporo, Tsukuba, Naha, and Kagoshima, Japan site are included as part of an agreement with the Japan Meteorological Agency and Hideyuki Sasaki.  These are standard on-going releases, which have a data sharing agreement with TRACE-P (see Section 2.4.4 and Appendix M).  The ozonesondes at Java, Indonesia; Fiji; and American Samoa are maintained by SHADOZ (Southern Hemisphere ADditional OZonesondes) and provided to TRACE-P through PI Anne Thompson.  The ozonesonde data at Hong Kong and Taiwan are provided to TRACE-P per agreements described in Sections 2.4.2 and 2.4.6, respectively.  Data sharing will conform to the TRACE-P Data Protocol (see Section 6.1).

Table 5.3-1 lists the investigator and/or organization responsible for ozonesonde operations at each site as well as the nominal launch rate

 

Table 5.3-1 TRACE-P Ozonesonde Network

SITE

INVESTIGATOR

1Trinidad Head, California

Sam Oltmans/NOAA

1Hilo, Hawaii

Sam Oltmans/NOAA

2Sapporo, Japan

Hideyuki Sasaki/JMA

2Tsukuba, Japan

Hideyuki Sasaki/JMA

2Naha, Japan,

Hideyuki Sasaki/JMA

2Kagoshima, Japan

Hideyuki Sasaki/JMA

3Java, Indonesia

SHADOZ

3Fiji

SHADOZ

3American Samoa

SHADOZ

4Hong Kong

H. K. Lam/HKO

5Taiwan

Jen-Ping Chen/NTU

6Cheju Island, Korea

Jae Kim/Pusan University

Launch Rate: 

1Once per week early spring 2000 – spring 2002, three times per week during the mission
2Once per week from as soon as possible through October 2001
3Weekly
4Once per week premission through May 2002, twice per week during deployment
5Once per week March 2000 – May 2002, twice per week during deployment
6Rate unknown

 

5.4 Meteorological Support Measurements

Meteorological support for flight planning will be provided by a team of meteorologists from the Massachusetts Institute of Technology (MIT), Florida State University (FSU), Hong Kong Observatory (HKO), Yokota Air Force Base (YAB), and the GTE Project Office. The Co-Mission Meteorologists from MIT and FSU (see Table 3.0-1) will, respectively, travel with and provide the specific meteorological support required for the P-3B and DC-8 aircraft. Personnel from HKO and YAB will provide general forecasting assistance during deployment from Hong Kong and Japan. ECMWF gridded data will be used during the entire mission for real-time forecasting and post-mission analysis. The GTE Project meteorologist will support the DC-8 and P-3B mission meteorologists through the acquisition and the preliminary analysis of meteorological data products.

FSU will serve as the "home base" for accessing the primary meteorological data products supporting flight planning during the aircraft deployment. Personnel from both MIT and FSU will use ECMWF gridded data to generate daily meteorology products for the field mission. Additionally, satellite imagery and meteorology products from various WWW sites will be used during the field mission. All collected and generated meteorology products will be stored on a dedicated PC located at each location, and a subgroup of these products will be stored on the "home base" PC for transmission to the field. A portable IMARSAT-B satellite-based communication system coupled to a "remote-base" PC will provide the communication link for a high data rate (56/64 KBPS) PC-to-PC transfer of the meteorology products (e.g. calculated and satellite images) stored on the "home base" PC located at FSU.

MIT will generate a set of forecast products to include maps of surface pressure, temperature and winds, divergent wind component at 1000 and 200 hPa, geopotential height and temperature, specific humidity, potential vorticity, vertical motion, and streamlines all at various pressure levels. FSU will calculate backward trajectories during the deployment phase using the ECMWF gridded data. Clusters of arrival points will be selected at locations along the anticipated flight tracks of the next several DC-8 and P-3B missions. Ten-day backward trajectories will be computed at various altitudes for each of these arrival points. A computer set up at the NASA Langley Research Center will automatically collect daily satellite imagery and meteorology products from various WWW sites, and download 3-hourly, 4-km, visible, infrared, and water vapor McIDAS satellite imagery files from the NASA Marshall Space Flight Center during the field mission.

After the deployment phase is completed, MIT, FSU, and the GTE Project Office will provide post-mission analyses. FSU will re-compute trajectories, using actual flight information to select the arrival points and levels. The Science Team will be asked to select additional locations/levels that are needed in their individual research analyses. These results will constitute the final trajectory archive located at the GTE Project Office at NASA Langley. Finally, trajectory climatology will be prepared for the Western Pacific Basin, emphasizing locations visited by the two aircraft. These results will also become part of the final archive. Table 5.4-1 lists the meteorological parameters that will be used for in-field flight planning, post-mission data analysis, and become part of the mission data archive located at the GTE Project Office at NASA Langley.

Table 5.4-1 Meteorological Parameters Required for Flight Planning/Data Analysis

MAPS

Parameter

Location

Pressure

Surface

Temperature

Surface

Wind

Surface

Divergent wind component

1000 and 200 hPa

Geopotential height

500 and 300 hPa

Temperature

500 and 300 hPa

Specific humidity

1000, 500, and 300 hPa

Potential vorticity

305, 315, 325, and 350K theta surfaces

Wind

305, 315, 325, and 350K theta surfaces

Vertical motion

850, 500, and 300 hPa

Streamlines

1000, 500, and 300 hPa

Specific humidity

Cross-section

Wind

Cross-section

Potential temperature

Cross-section

Potential vorticity

Cross-section


SATELLITE IMAGES

Satellite Images for planned flight track regions


TRAJECTORIES

Real time trajectories

Post mission trajectories+

Trajectory climatology+

Streamline, pressure, etc. climatology+

                                      + Available post mission

5.5 Supporting Ground Measurements

The Japanese ground station measurements by Koike and ozonesondes launched from Hawaii and California by Oltmans are self contained operations and are generally performed independently of the DC-8 and P-3B aircraft flights. These two activities do coordinate their measurements in the time interval of the planned aircraft flights and likely will coordinate to the specific over flight time of day if, and when, the aircraft are in the same area.

 

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