Results 121 to 130 of about 7,767 (239)

Chemistry: Space resources for teachers including suggestions for classroom activities and laboratory experiments [PDF]

open access: yes, 1971
Curriculum supplement to assist general chemistry teachers in updating instruction materials with aerospace ...
Bowman, W. H., Lawrence, R. M.
core   +1 more source

Propellant variability assessment [PDF]

open access: yes
Efforts to determine whether rocket propellant density and modulus can be reliably measured using non-destructive ultrasonic techniques are reported.
Schad, Kristin, Tytula, Thomas P.
core   +1 more source

Method of igniting solid propellants Patent [PDF]

open access: yes, 1966
Method for igniting solid propellant rocket motors by injecting hypergolic ...
Allen, H., Jr.   +2 more
core   +1 more source

Exploring in aerospace rocketry. 6 - Solid-propellant rocket systems [PDF]

open access: yes
Solid propellant rocket systems design and combustion efficiency and burning rate of solid ...
Mc Bride, J. F.
core   +1 more source

Advanced propulsion concepts for orbital transfer vehicles [PDF]

open access: yes
Studies of the United States Space Transportation System show that in the mid-to-late 1990s expanded capabilities for Orbital Transfer Vehicles (OTV) will be needed to meet increased payload requirements for transporting materials and possible men to ...
Cooper, L. P.
core   +1 more source

Improving the Mechanical Properties of Composite Rocket Propellants

open access: yes, 2004
Solid composite rocket propellants usually contain ammoniumperchlorate embedded in an elastic polymer binder. The bindercan be based on a liquid prepolymer such as hydroxyl-terminatedpolybutadiene, HTPB, or poly(3-nitratomethyl-3-methyl oxetane,PolyNIMMO.
openaire   +1 more source

Space storable thrustor investigation Final report [PDF]

open access: yes
Design and performance of space storable liquid FLOX methane thrustor of refractory composite ...
Coulbert, C. D., Fiorito, R. J.
core   +1 more source

Hydroxy-terminated polyether binders for composite rocket propellants

open access: yes, 2007
Propellants based on cross-linked Hydroxy Terminated PolyEther (HTPE) binders are being used as alternatives to Hydroxy Terminated PolyButadiene (HTPB) compositions. HTPE propellants have similar mechanical properties to HTPB propellants but they give a less severe response in ‘slow cook-off’ tests for IM compliance. A literature review is presented on
openaire   +1 more source

Advanced Solar-propelled Cargo Spacecraft for Mars Missions [PDF]

open access: yes
Three concepts for an unmanned, solar powered, cargo spacecraft for Mars support missions were investigated. These spacecraft are designed to carry a 50,000 kg payload from a low Earth orbit to a low Mars orbit.
Auziasdeturenne, Jacqueline   +9 more
core   +1 more source

Investigation of resin systems for improved ablative materials Interim report, 10 Jan. - 1 Jul. 1966 [PDF]

open access: yes
Preparation, and evaluation of polyimide sulfone resins, graphite-silica reinforced polyamide resins, and resin resistance to FLOX- methane, and fluorine-hydrogen ...
Burns, E. A.   +3 more
core   +1 more source

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