Results 81 to 90 of about 21,974 (173)

Thrust vector control study for large /260 inch/ rocket motor applications [PDF]

open access: yes
Design concepts of thrust vector control for large rocket motor ...
Erickson, L. H.   +3 more
core   +1 more source

High temperature NASP engine seal development [PDF]

open access: yes
Key to the development of advanced hypersonic engines such as those being considered for the National Aerospace Plane (NASP) is the development and evaluation of high temperature, flexible seals that must seal the many feet of gaps between the ...
Melis, Matthew E.   +3 more
core   +1 more source

S-cubed-a spacecraft and experiment description [PDF]

open access: yes
The launch of the Explorer 45 satellite and the instruments installed in the satellite are discussed. The scientific objectives of the first mission, the orbital parameters, and the capabilities of the data system are examined.
Hoffman, R. A., Longanecker, G. W.
core   +1 more source

Study of a thrust vectoring system for rockets through a pressurized air test bench

open access: yes, 2017
Aiming to be the first step towards the design of a fully operational stabilization system for rockets, thebuilding of a model is done representing the attitudeof a rocket with anactive stability system. Several tests are done with the model both static and dynamic with different type of sensors that give us a view of the response of the system to ...
openaire   +1 more source

Hydrogen film cooling of a small hydrogen-oxygen thrust chamber and its effect on erosion rates of various ablative materials [PDF]

open access: yes
An experimental investigation was conducted to determine what arrangement of film-coolant-injection orifices should be used to decrease the erosion rates of small, high temperature, high pressure ablative thrust chambers without incurring a large penalty
Hannum, N.   +2 more
core   +1 more source

Hybrid propulsion technology program: Phase 1. Volume 3: Thiokol Corporation Space Operations [PDF]

open access: yes
Three candidate hybrid propulsion (HP) concepts were identified, optimized, evaluated, and refined through an iterative process that continually forced improvement to the systems with respect to safety, reliability, cost, and performance criteria. A full
Schuler, A. L., Wiley, D. R.
core   +1 more source

Space Physics Group quarterly status report [PDF]

open access: yes
Calibrating prototype gamma ray detector for OSO-

core   +1 more source

Development of P4.1 Altitude Simulation for VINCI Engine [PDF]

open access: yes, 2005
Böhm, Christian   +3 more
core  

Canister for Producing TMA Trails in the Upper Atmosphere [PDF]

open access: yes
Payload canister for producing trimethyl aluminum trails in upper atmosphere using Nike-Cajun or Nike-Apache ...
Corman, A., Guarino, N. J.
core   +1 more source

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