Guided Missile and Space Vehicle Propulsion Unit and Propulsion Unit Parts Manufacturing

MK7 SHIPSETS TWCP HEATSHIELD

THE PURPOSE OF THIS EFFORT IS THE DESIGN, MANUFACTURING, AND DEVELOPMENT TESTING FOR LOW LEAKAGE VALVES CONCEPTS USED TO PRIMARILY SERVICE LIQUID HYDROGEN IN-SPACE APPLICATIONS. THESE IN-SPACE APPLICATIONS INCLUDE ENVISIONED DEEP SPACE TRANSPORTATION

FIRST DDT AND E, ARES I-X, AND FLIGHT TESTS. FIRST STAGE WILL BE A FIVE SEGMENT, SOLID ROCKET BOOSTER DERIVED FROM THE SPACE SHUTTLE PROGRAM (SSP) SOLID ROCKET BOOSTER (SRB)/REUSABLE SOLID ROCKET MOTOR (RSRM). THE CONTRACTOR SHALL FURNISH THE NECESSARY MANAGEMENT, ENGINEERING, LABOR, FACILITIES, TOOLS, EQUIPMENT, AND MATERIALS REQUIRED FOR FIRST STAGE DEVELOPMENT, QUALIFICATION, CERTIFICATION AND ACCEPTANCE PROGRAM. ACTIVITIES INCLUDE: REDESIGN AND TESTING OF THE MOTOR TO INCORPORATE THE FIFTH SEGMENT AND PRODUCTION OF FIVE FULL SCALE GROUND STATIC TEST MOTORS: TWO DEVELOPMENT MOTORS (DMS)-AND THREE QUALIFICATION MOTORS (QMS); STRUCTURAL TEST ARTICLE (STA), GROUND VIBRATION TEST MOTORS (GVTMS) AND OTHER DEVELOPMENT TESTING; REDESIGN OF THE AVIONICS, DECELERATION, SEPARATION, AND FLIGHT TERMINATION SYSTEM (FTS) SUBSYSTEMS; ARES I-X: SIMULATED ARES I OUTER MOLD LINE/MASS PROPERTIES USING MODIFIED SRB/RSRM; AND THREE FLIGHT TEST VEHICLES. TAS::80 0124::TAS

CLAMP, SEPARATION

THIS TASK ORDER PROCURES A VARIETY OF TESTS FOR MINUTEMAN (MM) AND PEACEKEEPER (PK) ROCKET MOTOR SUSTAINMENT.

THIS TASK ORDER PROCURES A STUDY FOR THE DESIGN AND DEVELOPMENT OF THREE (3) HYDRAULIC TEST CARTS TO BE USED FOR AGING SURVEILLANCE (AS) SUSTAINMENT EFFORTS

ANTENNA WINDOW FABRICATION

EMBEDDED ENTREPRENEUR INITIATIVE (EEI) + MVP OPTION

ORIOLE ROCKET MOTORS (ORM) AND THRUST VECTOR CONTROL (TVC) SYSTEMS WITH ANCILLARY HARDWARE AND SHIPPING CONTAINERS FOR TESTING AT WHITE SANDS MISSILE RANGE.

DELIVERY ORDER 002 - EQUIPMENT PURCHASE