Spiral

Main Propulsion
Test Article  (MPTA-098)

Background

The Main Propulsion Test Article (MPTA-098) consisted of an Orbiter aft-fuselage, a trus arrangement which simulated the Orbiter mid-fuselage and a complete Space Shuttle Main Engine (SSME) thrust structure including all main propulsion system plumbing and electrical systems. The unit was shipped to the National Space Technology Laboratory (NSTL) on 06/24/77 where it was mated with the Main Propulsion Test Article External Tank (MPTA-ET) and used for static engine tests. The MPTA-ET is now located at the Marshall Space Flight Center (MSFC) Alabama Space and Rocket Center where it is mounted to the "Orbiter Simulator" Pathfinder while MPTA-098 is at the Stennis Space Center (SSC) in Mississippi (previously called the NSTL).

On 7/2/79, MPTA-098 suffered major structural damage due to a fractured fuel valve on engine 2002. Testing resumed two months later but a liquid oxygen high speed turbopump failed 9.7 seconds into a scheduled 510 second test. It wasn't until 12/17/79 that a complete static firing was accomplished that included 3 main engines running up to 100 percent of rated thrust for 554 seconds.

On 1/17/81, just three months prior to the scheduled STS-1 launch date, MPTA-098 successfully demonstrated a 625 second firing. The three flight rated engines from Columbia were removed, shipped to NSTL, and installed on MPTA-098 where they successfully completed a 520-second flight mission demonstration test. The engines were then shipped back to KSC and installed on Columbia where they successfully performed a 20-second Flight Readiness Firing (FRF) on 2/20/81. This cleared the way for the launch of STS-1 on 4/12/81.

Construction Milestones (MPTA-098)

07/26/72
07/17/74
06/24/75
01/23/76
03/17/76
05/03/76
06/29/76
07/08/76
07/12/76
07/24/76
05/27/77
06/03/77
06/24/77
09/10/77
Contract Award
Start of long lead fabrication
Start structural assembly of aft-fuselage
Truss on dock at Rockwell Downey
Complete premate at Downey and delivered to Palmdale
Complete proof load test setup at Palmdale
Move truss assembly from Palmdale Building 294 to 295
MPTA-098 on dock at Downey
Start of Final Assembly
Complete MPTA-098 proof load test
Completed Final Assembly, Transport to Seal Beach
Transport from Seal Beach to NSTL
Arrival at NSTL for static firing
Arrival of MPTA-ET at NSTL

Testing Milestones (MPTA-098)

04/21/78
05/19/78
06/15/78
07/07/78
05/04/79
06/12/79
10/24/79
11/04/79
12/17/79
02/28/80
03/28/80
04/16/80
05/30/80
07/12/80
11/03/80
12/04/80
01/17/81
1st static firing (2.5 sec)
2nd static firing (15 sec)
3rd static firing (50 sec)
4th static firing (100 sec)
5th static firing flight nozzles (1.5 sec)
5th static firing flight nozzles (54 sec)
6th static firing flight nozzles (scrubbed)
6th static firing flight nozzles (10 sec cutoff)
6th static firing non-flight (554 sec)
7th static firing non-flight (555 sec)
8th static firing non-flight (539 sec)
9th static firing non-flight (4.6 sec cutoff)
9th static firing non-flight (565 sec cutoff)
10th static firing flight nozzels (105 sec shutdown)
11th static firing flight nozzels (20 sec shutdown)
11th static firing non-flight (591 sec)
12th static firing flight nozzels (625 sec)

Pages mainteinded by
Claudio Ariotti, IK1SLD



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