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SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
WAVE Organization Chart
Management and Integration
M. RossAerospace Corp
WB-57 Program OfficeA. RobertsNASA-JSC
Mission PlanningM. Ross
Aerospace Corp
Camera and OpticsR. Grubbs
NASA-MSFC
camera systemoptical systemsIPWG InterfaceData Recording
Optical Bench assemblycamera boresighting
operation documentationSEO monitorsData delivery
Optical Systems Budget Mgmt
Turret and Tracking System J. Collier
Southern Research Institute
Aircraft OperationsAircraft Engineering
Aircraft System ReviewOperator Interface Req
Deployment ManagementBudget Managemente
Imagery SimulationsRange Interface
Flight path definitionMission Planning
mission documentationintegration and test palnning
CFD modelingRequirements
Interface documentationAircraft Interface
SEO controlsTracking System
Point/track calibrationMaintenance support planoperation documentation
operatior training
IPWGShuttle Program Office
S R
PUMA sits here, Toohey as Mission
scientist
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
Approximate Mission Timeline
L - 5 days integra te and checkout sensors a t EFD L - 3 days Opera tiona l Re adine ss Review a t EFB L - 2 days fe rry both a ircraft from EFD to Pa trick AFB L - 1 day MRR at PAFB fina l se nsor checks and configura tion L - 05:30:00 hands off a ircraft L - 02:30:00 a ircra ft takeoff from Pa trick AFB L - 02:00:00 a ircra ft ente r holding pa tte rns and ve rify communica tions with ROCC L - 00:07:30 a ircra ft begin fina l lag toward liftoff pos itions L - 00:00:00 liftoff L + 00:02:08 SRB separa tion L + 00:03:51 nega tive re turn L + 00:08:24 MECO L + 00:25:00 [approximate RTLS landing] L + 01:30:00 a ircra ft land a t Pa trick AFB L + 03:00:00 da ta ready for de live ry L + 24:00:00 re turn ferry both a ircra ft to Ellington Fie ld
TBDDyncorp and SRIdeployment sched
PUMA intercepts inthis window
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
Mission Timelineexample 1200 launch
Aircraftto PAFB
MRR(PAFB)
SensorPreflights
Mission
0000
L+ 1.5L-2.5
2400
climb to altitude P1 P2 P3 P4 P5 return and descent landand
downloaddata
launch
handson mission
handsoff
L - 7.5 L - 2.5 L + 1.5
L - 2 day L - 1 day L - 0 day
sensor checklists
PUMA
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
WAVE A Mission
• Atlas IIAS: 19 May
• Validated aircraft ops at PAFB- two aircraft support- associated instruments
• Determined range support process- path to ER approval- required MSR documentation- deadlines
• Lessons learned- figure 8 difficult to manage- takeoff at L - 2.5- define ROCC rep function- launch slip management
Plume in GOES image
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
WAVE-A Flight: Figure-8 holding pattern
Plume intercepts
• Pass 4 (T+18 min)
• 12.6 km
• CO2 at 10 Hz (oversampled)
• JPL H2O at 0.8 Hz
• Will add particles and CLH H2O
Comparison of waterInstruments
• CU particulate water at 2 Hz (arbitrary units)
• JLH at 0.8 Hz (ppm)
• No enhancements observed, consistent with low RH
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
November 2004
S M T W T F S
1 2 3 4 5 6
7 8 9 10 11 12 13
14 15 16 17 18 19 20
21 22 23 24 25 26 27
28 29 30
December 2004
S M T W T F S
1 2 3 4
5 6 7 8 9 10 11
12 13 14 15 16 17 18
19 20 21 22 23 24 25
26 27 28 29 30 31
January 2005
S M T W T F S
1
2 3 4 5 6 7 8
9 10 11 12 13 14 15
16 17 18 19 20 21 22
23 24 25 26 27 28 29
30 31
February 2004
S M T W T F S
1 2 3 4 5 6 7
8 9 10 11 12 13 14
15 16 17 18 19 20 21
22 23 24 25 26 27 28
29
WAVE/PUMA ELV Intercept Opportunities
PUMA will focus on December and February
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
Integration Schedule
Ju ly Aug Se pt O ct Nov De c Jan Fe b M ar Apr M ay Jun
Ele ctr ica l De sig n an d F ab
Ele ctr ica l Ha rn ess in 9 26
Ele ctr ica l Ha rn ess in 9 28
Stre ss An a lysis an d Re virew
Ae ro d yna mics An a lysis an d Re vie w
No se se a l F ab a nd test
P ito t-Sta tic T esting 9 26
Pito t-Sta tic T esting 9 28
W AVE B O R R
W AVE B (9 2 6 a n d 92 8)
Se nsor 1 In te gra tion a nd T e st
W AVE C O RR
W AVE C (92 6 )
Se nsor 2 In te gra tion a nd T e st
T ra in in g a n d Pro fic ie ncy F lig h ts
IO C
IO C
PUMA B (test flights)PUMA C (ELV intercepts)
Shuttle Return to Space
SOUTHERN RESEARCH
SYSTEMS DEVELOPMENT DEPARTMENT
I N S T I T U T E
Sensor 1 Flight Test Plan
FT3 (5 hr, high altitude)expand envelope of pressure and temperature control tracking system operations and performance testingoptical performance testing
FT4 (5 hr. low and high altitude)simulate WAVE B mission operations tracking system operations testingoptical performance testingT-38 tracking test
FT1 (2 hr, mid altitude)validate checklistdata collect: aerodynamic effects at varying α, β, Q and turret orientationsinvestigate pressure and temperature control verify turret motion and control verify camera and recorder function and control
FT2 (3 hr, mid and high altitude)expand envelope of aerodynamic effects at varying α, β, Q and turret orientationsexpand envelope of pressure and temperature control verify tracking system mode functions and control benchmark system optical performance