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.
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.
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 |
|
|
|
Begin install inlets and plumbing |
|
|
|
|
|
|
08 |
Racks avail. to begin installation |
|
|
Racks avail. to begin installation |
|
|
|
|
|
|
15 |
Holiday |
|
|
Holiday |
|
|
Holiday |
|
|
23 Jan |
CCB Hazard Review | |||||||||
|
25 |
|
|
Complete Rack Install and C/O. |
|
|
|
|
|
|
26 Jan |
Complete Rack Install and C/O |
|||||||||
|
29 |
Wallops |
|
|
Tech Brief |
|
|
|
|
|
|
30 |
Wallops |
|
|
Cmplt. Elect/DADS & Power Ck |
|
|
|
|
|
|
31 |
Wallops |
|
|
Rollout, Wt. & Balance, etc |
|
|
|
|
|
|
01 |
Wallops |
|
|
Engineering Check & ICATS Flight |
|
2 |
|
|
|
|
02 |
Wallops |
|
|
Pilot Proficiency Flight |
|
|
|
|
|
|
03 |
Wallops |
|
|
Laser Calibrations |
|
|
|
|
|
|
04 |
Wallops |
|
|
Laser Calibrations |
|
|
|
|
|
|
05 |
Wallops |
|
|
ICATS RVSM cert. Flight |
|
|
|
|
|
|
06 |
Complete power check and hazard analysis |
|
2 |
Laser Calibrations |
|
|
|
|
|
|
07 |
Safety brief and FRR |
|
|
Laser Calibrations |
|
|
|
|
|
|
08 |
Engineering Check Flight |
|
2 |
Laser Calibrations |
|
|
|
|
|
|
09 |
Test Flight 1 |
|
2.5 |
Laser Calibrations |
|
|
|
|
|
|
10 |
Wallops |
|
|
Laser Calibrations |
|
|
|
|
|
|
11 |
Wallops |
|
|
Dryden |
|
|
|
|
|
|
12 |
Test Flight 2 |
|
3.5 |
Mandatory Safety Briefing |
|
|
|
|
|
|
13 |
Wallops |
|
|
Dryden |
|
|
|
|
|
|
14 |
Wallops |
|
|
Test Flight 1 |
|
3 |
|
|
|
|
15 |
Test Flight 3 |
|
5.5 |
ORR |
|
|
|
|
|
|
16 |
C-130 load ready in N-159 |
|
|
Test Flight 2 |
|
4 |
|
|
|
|
17 |
Wallops |
|
|
Dryden |
|
|
|
|
|
18 Feb |
Wallops |
Dryden |
||||||||
|
19 |
Holiday--Wallops Pack |
|
|
Holiday |
|
|
Holiday |
|
|
|
20 |
Wallops Pack & Load C-130 |
|
|
Test Flight 3 |
|
6 |
Upload P-3B Equipment |
|
|
|
21 |
Wallops Pack & Load C-130 |
|
|
Dryden Pack |
|
|
Upload P-3B Equipment |
|
|
|
22 |
Delay |
|
Dryden Pack |
|
|
Delay |
|
|
|
|
23 |
Delay |
|
|
Dryden Pack & load C-130 |
|
|
Transit: Wallops to Dryden |
7.9 |
7.9 |
24 |
Transit: Wallops to Palmdale |
6.8 |
8.5 |
Dryden Pack |
|
|
Transit: DFRC to Palmdale |
0.4 |
0.4 |
|
25 |
Palmdale |
|
|
Dryden Pack |
|
|
Palmdale |
|
|
|
27 |
26 |
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 |
27 |
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 |
28 |
Wake Island |
|
|
Guam |
|
|
Wake Island |
|
|
02 |
01 |
Transit: Wake Island to Guam |
4.1 |
6 |
Guam |
|
Transit: Wake Island to Guam |
4.7 |
4.7 |
|
03 |
02 |
Guam |
|
|
Guam |
|
|
Guam |
|
|
04 |
03 |
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 |
04 Mar |
Hong Kong |
|
Hong Kong |
|
|
Offload all equipment |
|||
06 |
05 |
Hong Kong Local 1 |
|
8 |
Hong Kong Local 1 |
10 |
|
|
|
|
07 |
06 |
Down Day |
|
|
Down Day |
|
|
|
|
|
08 |
07 |
Hong Kong |
|
8 |
Hong Kong |
|
8 |
|
|
|
09 |
08 |
Hong Kong Local 2 to Okinawa |
2.7 |
8 |
Hong Kong Local 2 to Okinawa |
2.1 |
10 |
|
|
|
10 |
09 |
Hong Kong Local 3 Okinawa to Hong Kong |
2.9 |
8 |
Hong Kong Local 3 Okinawa to Hong Kong |
2.3 |
6 |
|
|
|
11 |
10 |
Hong Kong |
|
|
Hong Kong |
|
|
|
|
|
12 |
11 |
Hong Kong |
|
|
Hong Kong |
|
|
|
|
|
13 |
12 |
Hong Kong Local 4 |
|
8 |
Hong Kong Local 4 |
|
8 |
|
|
|
14 |
13 |
Hong Kong |
|
|
Hong Kong |
|
|
|
|
|
15 |
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 |
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 |
19 |
Yokota AB |
|
|
Yokota AB crew changeout |
|
|
|
|
|
21 |
20 Mar |
Yokota Local 1 |
|
8 |
Yokota Local 1 |
|
8 |
|
|
|
22 |
21 |
Down Day |
|
|
Down Day |
|
|
|
|
|
23 |
22 |
Yokota AB |
|
|
Yokota AB |
|
|
|
|
|
24 |
23 |
Yokota Local 2 |
|
8 |
Yokota Local 2 |
|
8 |
|
|
|
25 |
24 |
Yokota AB |
|
|
Yokota AB |
|
|
|
|
|
26 |
25 |
Yokota AB |
|
|
Yokota AB |
|
|
|
|
|
27 |
26 |
Yokota Local 3 |
|
6 |
Yokota Local 3 |
|
8 |
|
|
|
28 |
27 |
Yokota AB |
|
|
Yokota AB |
|
|
|
|
|
29 |
28 |
Yokota AB |
|
|
Yokota AB |
|
|
|
|
|
30 |
29 |
Yokota Local 4 Yokota to Okinawa |
3 |
8 |
Yokota Local 4 Yokota to Okinawa |
2.3 |
10 |
|
|
|
31 |
30 |
Yokota Local 5 Okinawa to Yokota |
2.7 |
8 |
Yokota Local 5 Okinawa to Yokota |
2.1 |
8 |
|
|
|
01 |
31 |
Down Day |
|
Down Day |
|
|
|
|
|
|
02 |
01 Apr |
Yokota Pack |
|
Yokota Pack |
|
Upload all P-3B Equipment |
||||
03 |
02 |
Yokota Pack |
|
|
Yokota Pack |
|
|
Upload all DC-8 Equipment |
|
|
04 |
03 |
Transit: Yokota AB to Midway |
5.5 |
8 |
Transit: Yokota AB to Kona, Hawaii |
8.5 |
10 |
Transit: Yokota AB to Midway |
6.2 |
6.2 |
05 |
04 |
Midway |
|
|
Kona |
|
|
Midway |
|
|
|
05 |
Midway Local 1 |
|
8 |
Kona Local 1 |
|
10 |
Midway |
|
|
|
06 |
Midway Pack |
|
|
Down Day |
|
|
Midway |
|
|
|
07 |
Transit: Midway to Kona, Hawaii |
3.2 |
4 |
Kona Pack |
|
|
Transit: Midway to Kona, Hawaii |
3.6 |
3.6 |
|
08 |
Kona, Hawaii |
|
|
Kona, Hawaii |
|
|
Reload and Upload DC-8 |
|
|
|
09 |
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 |
Transit: Dryden to WFF |
5.3 |
7 |
Off Load |
|
|
Transit: Dryden to WFF |
6 |
6 |
|
11 |
Off Load |
|
|
Off Load |
|
|
Off Load P-3B Equipment |
|
|
|
12 |
Off Load |
|
|
Off Load |
|
|
Off Load P-3B Equipment |
|
|
|
13 |
Off Load |
|
|
Complete |
|
|
Complete |
|
|
|
14 |
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
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 for planned flight track regions |
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.