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    Development of Cost-Optimized Insulation System for Use in Large Solid Rocket Motors. Volume 2, Task 2 - Process Evaluation Final Report

    D. L. Nachbar / B. A. Simmons | NTIS | 1969
    Schlagwörter: Solid propellant rocket engines

    Some Typical Solid Propellant Rocket Motors

    B. T. C. Zandbergen | NTIS | 1995
    Schlagwörter: Solid propellant rocket engines , Solid propellant combustion

    Guided Missile Propulsion System Hazards of Electromagnetic Radiation to Ordnance (Hero) RF Characteristics of Electro-Explosive Devices

    NTIS | 1964
    Schlagwörter: Rocket motors (Solid propellant)

    Development of Cost-Optimized Insulation System for Use in Large Solid Rocket Motors. Volum 3, Task 3 - Material Performance Determination Final Report

    D. L. Nachbar / B. A. Simmons | NTIS | 1969
    Schlagwörter: Solid propellant rocket engines

    Sts Spin-Stabilized Upper Stage Study (Study 2.6). Volume 2: Technical Report

    NTIS | 1975
    Schlagwörter: Solid propellant rocket engines

    Weapon System 133A. Program Progress Production Motors. Stage I Minuteman

    NTIS | 1966
    Schlagwörter: Solid propellant rocket engines

    Development of Cost-Optimized Insulation System for Use in Large Solid Rocket Motors. Volume 4, Task 4 - 260 in. Dia Motor Insulation System Design and Process Plan Final Report

    D. L. Nachbar / B. A. Simmons | NTIS | 1969
    Schlagwörter: Solid propellant rocket engines

    Development of Cost-Optimized Insulation System for Use in Large Solid Rocket Motors. Volume 1, Task 1 - Survey and Screening Final Report

    D. L. Nachbar / B. A. Simmons | NTIS | 1969
    Schlagwörter: Solid propellant rocket engines

    Feasibility, Parametric Design, and Comparative Analysis of an Unguided Solid Fuel Rocket Vehicle with Solar Orbit, Earth Probe, and Re-Entry Mission Capabilities

    T. C. Walker | NTIS | 1967
    Schlagwörter: Solid propellant rocket engine

    Thiokol 260-Sl Subscale Nozzle Verification Program, 65-SS-2 and 65-SS-3 Motors

    NTIS | 1966
    Schlagwörter: Solid propellant rocket engines

    Solid-Propellant Combustion Instability Suppression Devices. Volume II. Survey of Applications of Mechanical Suppression Devices in Solid-Propellant Rockets

    W. G. Haymes / W. T. Brooks / W. M. Burkes | NTIS | 1972
    Schlagwörter: Solid propellant rocket engines

    Weapon System 133A. Program Progress Production Motors Stage I Minuteman

    NTIS | 1966
    Schlagwörter: Solid propellant rocket engines

    Probabilistic Risk Assessment of the Space Shuttle. Phase 3: A Study of the Potential of Losing the Vehicle During Nominal Operation. Volume 4: System Models and Data Analysis

    J. R. Fragola / G. Maggio / M. V. Frank et al. | NTIS | 1995
    Schlagwörter: Solid propellant rocket engines

    Liquid Rocket Booster (LRB) for the Space Transportation System (STS) Systems Study. Appendix C: Battery Report for the Liquid Rocket Booster TVC Actuators

    NTIS | 1989
    Schlagwörter: Solid propellant rocket engines

    Design, Test, and Documentation of the Marc 36 A1, 1KS-75 Spin Motor for the Scout Vehicles

    NTIS | 1966
    Schlagwörter: Solid propellant

    Aeroheating (Pressure) Characteristics on a 0.010-Scale Version of the Vehicle 3 Space Shuttle Configuration (26-Ots) in Langley Research Center 4-Foot Wind Tunnel (IH4)

    R. B. Kingsland | NTIS | 1976
    Schlagwörter: Solid propellant rocket engines

    Aeroheating (Pressure) Characteristics on a 0.010-Scale Version of the Vehicle 3 Space Shuttle Configuration (26-Ots) in the Langley Research Center 4-Foot Wind Tunnel (IH4)

    R. B. Kingsland | NTIS | 1976
    Schlagwörter: Solid propellant rocket engines

    260-IN.-Dia Motor Feasibility Demonstration Program Final Program Summary Report, Jun. 1963 - Apr. 1966

    NTIS | 1966
    Schlagwörter: Solid propellant rocket engine

    Study of Selected Thrust Vector Control Systems for Solid Propellant Motors Final Report, 2 Jun. - 2 Aug. 1965

    NTIS | 1965
    Schlagwörter: Solid propellant rocket engine

    Development of a Filament Wound Case Design for Solid Propellant Rocket Motors in the 260-Inch Diameter Class Final Report

    C. W. Vogt | NTIS | 1969
    Schlagwörter: Solid propellant rocket engines

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