WAVE Organization Chart

Size: px

Start display at page:

Download "WAVE Organization Chart"

Darrell Glenn
5 years ago
Views:

PUMA sits here, Toohey as Mission scientist WAVE Organization Chart Management and Integration M. Ross Aerospace Corp IPWG Shuttle Program Office WB-57 Program Office A.

1 PUMA sits here, Toohey as Mission scientist WAVE Organization Chart Management and Integration M. Ross Aerospace Corp IPWG Shuttle Program Office WB-57 Program Office A. Roberts NASA-JSC Mission Planning M. Ross Aerospace Corp Camera and Optics R. Grubbs NASA-MSFC R Turret and Tracking System J. Collier Southern Research Institute Aircraft Operations Aircraft Engineering Aircraft System Review Operator Interface Req Deployment Management Budget Managemente Imagery Simulations Range Interface Flight path definition Mission Planning mission documentation integration and test palnning CFD modeling Requirements camera system optical systems IPWG Interface Data Recording Optical Bench assembly camera boresighting operation documentation SEO monitors Data delivery Optical Systems Budget Mgmt Interface documentation Aircraft Interface SEO controls Tracking System Point/track calibration Maintenance support plan operation documentation operatior training

2 Approximate Mission Timeline L - 5 days L - 3 days L - 2 days L - 1 day L - 05:30:00 L - 02:30:00 L - 02:00:00 L - 00:07:30 L - 00:00:00 L + 00:02:08 L + 00:03:51 L + 00:08:24 L + 00:25:00 L + 01:30:00 L + 03:00:00 L + 24:00:00 integrate and checkout sensors at EFD Operational Re a dine s s Review at EFB ferry both aircraft from EFD to Patrick AFB MRR at PAFB final s e nsor checks and configuration hands off a ircra ft aircraft takeoff from Patrick AFB aircraft enter holding patterns and verify communications with ROCC aircraft begin final la g toward liftoff pos itions liftoff SRB separation nega tive return MECO [approximate RTLS landing] aircraft land at Patrick AFB data ready for delivery return ferry both aircraft to Ellington Field PUMA intercepts in this window TBD Dyncorp and SRI deployment sched

3 Aircraft to PAFB Mission Timeline example 1200 launch MRR (PAFB) Sensor Preflights Mission L - 2 day L - 1 day L - 0 day 0000 hands on hands off mission 2400 L L L launch L-2.5 climb to altitude P1 P2 P3 P4 P5 return and descent land sensor checklists PUMA and download data L+ 1.5

4 Atlas IIAS: 19 May WAVE A Mission 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 define ROCC rep function - launch slip management

6 Plume in GOES image

7 WAVE-A Flight: Figure-8 holding pattern Plume intercepts

8 Pass 4 (T+18 min) 12.6 km CO 2 at 10 Hz (oversampled) JPL H 2 O at 0.8 Hz Will add particles and CLH H 2 O

9 Comparison of water Instruments CU particulate water at 2 Hz (arbitrary units) JLH at 0.8 Hz (ppm) No enhancements observed, consistent with low RH

10 WAVE/PUMA ELV Intercept Opportunities PUMA will focus on December and February November 2004 S M T W T F S December 2004 S M T W T F S January 2005 S M T W T F S February 2004 S M T W T F S

11 Integration Schedule July Aug Se pt Oct Nov De c Jan Fe b M ar Apr M ay Jun Ele ctrica l Design and Fab Ele ctrica l Harness in 926 Ele ctrica l Harness in 928 Stre ss Analysis and Revirew Ae rodynamics Analysis and Review No se seal Fab and test Pito t-sta tic Testing 926 Pito t-sta tic Testing 928 W AVE B ORR W AVE B (926 and 928) Se nsor 1 Integration and Test W AVE C ORR W AVE C (926) Se nsor 2 Integration and Test T rain in g and Proficiency Flights IO C IO C PUMA B (test flights) PUMA C (ELV intercepts) Shuttle Return to Space

12 Sensor 1 Flight Test Plan FT1 (2 hr, mid altitude) validate checklist data collect: aerodynamic effects at varying α, β, Q and turret orientations investigate 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 orientations expand envelope of pressure and temperature control verify tracking system mode functions and control benchmark system optical performance FT3 (5 hr, high altitude) expand envelope of pressure and temperature control tracking system operations and performance testing optical performance testing FT4 (5 hr. low and high altitude) simulate WAVE B mission operations tracking system operations testing optical performance testing T-38 tracking test

Lockheed SR-71B ( / NASA 831) Flight Log

Lockheed SR-71B ( / NASA 831) Flight Log NASA Dryden Flight Research Center History Office Lockheed SR-71B (61-7956 / NASA 831) Flight Log Compiled by Peter W. Merlin September 2002 NASA crews flew four Lockheed SR-71 airplanes between July 1991