[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Allred, 1995 - Google Patents

Quantitative evaluation of human-rating-The impact of solid propulsion on the reliability and safety of space launch vehicles

Allred, 1995

Document ID
12639556320796214035
Author
Allred A
Publication year
Publication venue
Space Programs and Technologies Conference

External Links

Snippet

Human-rating concerns can have a significant impact on vehicle cost and operability. If properly managed, this impact can be effectively minimized. These concerns must he addressed quantitatively beginning with the inception of a program. Assessment of …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • F02K9/343Joints, connections, seals therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/646Docking or rendez-vous systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • B64D25/08Ejecting or escaping means

Similar Documents

Publication Publication Date Title
Palaszewski et al. Launch vehicle performance using metallized propellants
US20120312927A1 (en) Launch abort and orbital maneuver system
WO2014022836A2 (en) Universal elliptical-sliced solid grain geometry and coupled grill-feedthrough featured assembly for solid rocket motor and coaxial hybrid rocket design
US7484692B1 (en) Integrated abort rocket and orbital propulsion system
Allred Quantitative evaluation of human-rating-The impact of solid propulsion on the reliability and safety of space launch vehicles
US20070012821A1 (en) Launch vehicle crew escape system
Arves et al. Development of a N2O/HTPB hybrid rocket motor
Allred et al. Crew survival and intact abort using solid rocket boosters
Allen Historical reliability of US launch vehicles
Lake et al. A Study of the Role of Pyrotechnic Systems on the Space Shuttle Program
Sauvageau et al. Launch vehicle historical reliability
Wiswell et al. X-15 propulsion system
Baker et al. Mars science laboratory descent-stage integrated propulsion subsystem: development and flight performance
Sarigul-Klijn et al. Concept and Design Details of a Universal Gas-Gas Launch Escape System
US12049855B1 (en) Method and apparatus for reducing consequences of a bulkhead failure for a liquid methane and liquid oxygen rocket
Vaughan Apollo reaction control systems
Allred et al. Human-rating aspects of solid propulsion
Go et al. Mission Success of US Launch Vehicle Flights from a Propulsion Stage-based Perspective: 1980-2015
Seeholzer Applications catalog of pyrotechnically actuated devices/systems
Lo et al. Hybrid boosters for Ariane 5
Maybee et al. A novel design warm gas pressurization system
Boorady et al. Solution of the high-vacuum hard-start problem of the IRFNA-UDMH rocket for Gemini Agena.
CHASE IUS flight motor designs and full-scale development program
CRAMER et al. Application of the integrated modular engine (IME) to space vehicle concepts
Cotta et al. Upper stage options for reusable launch vehicles