Results 141 to 150 of about 142,443 (296)

CHOOSING RATIONAL ENGINEERING SOLUTIONS AND DESIGN CRITERIA OF THROTTABLE SOLID FUEL ROCKET ENGINES

, 2022
С.В. Лавров, Б.К. Терпогосова   +1 more
openalex   +1 more source

Response of selected plant and insect species to simulated solid rocket exhaust mixtures and to exhaust components from solid rocket fuels [PDF]

The effects of solid rocket fuel (SRF) exhaust on selected plant and and insect species in the Merritt Island, Florida area was investigated in order to determine if the exhaust clouds generated by shuttle launches would adversely affect the native ...
Ambrose, J. T., Engle, M., Heck, W. W., Knott, W. M., Mccrimmon, J. N., Romanow, L. A., Sawyer, A. G., Stahel, E. P., Tyson, J. D.   +8 more
core   +1 more source

Space transportation systems, launch systems, and propulsion for the Space Exploration Initiative: Results from Project Outreach [PDF]

A number of transportation and propulsion options for Mars exploration missions are analyzed. As part of Project Outreach, RAND received and evaluated 350 submissions in the launch vehicle, space transportation, and propulsion areas.
Augenstein, B., Garber, T., Hiland, J., Miller, M., Orletsky, D.   +4 more
core   +1 more source

Chemically Collapsible Mandrel for Solid Rocket Motor Processing

Journal of Aerospace Technology and Management, 2015
Composite propellant mainly consists of two parts, binder matrix (prepolymer, plasticizer, cross linker, antioxidant and curative etc.) and solid ingredients (oxidizer, metal fuel, burn rate modifier, combustion stabilizer etc.).
Abhijit Dey, Arvind Kumar, Arun K Sikder, Manoj Gupta   +3 more
doaj  

A Unique Hybrid Propulsion System Design for Large Space Boosters [PDF]

A study was made of the application of hybrid rocket propulsion technology to large space boosters. Safety, reliability, cost, and performance comprised the evaluation criteria, in order of relative importance, for this study.
Rodgers, Frederick C.
core   +1 more source

Development of Wall Regression Model of Hybrid Rocket Solid Fuel

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 2016
Tsuyoshi Totani, Masashi Wakita, Kazuya Nawata, Nobuyuki Oshima, Harunori Nagata, Tatsuya Saito, Shunya Sasaki   +6 more
openaire   +3 more sources

Design issues for lunar in situ aluminum/oxygen propellant rocket engines [PDF]

Design issues for lunar ascent and lunar descent rocket engines fueled by aluminum/oxygen propellant produced in situ at the lunar surface were evaluated.
Meyer, Michael L.
core   +1 more source

Alpha particle detection in high magnetic fields with applications in designing fission fragment rocket engine. [PDF]

Sci Rep
Puri S, Lin C, Gillespie A, Jones I, Carty C, Kelley M, Weed R, Duncan RV.   +7 more
europepmc   +1 more source

Performance of a circular body earth-to-orbit winged transport with various strap-on boosters [PDF]

Various types of twin strap-on boosters were evaluated by applying them to a core vehicle. The core vehicle has a clipped delta wing and a simple circular body, and is equipped with five Space Shuttle main engines.
Macconochie, Ian O., Naftel, J. Chris, Widman, Frederick W.   +2 more
core   +1 more source

Design and Optimization of a Hybrid Gas Generator for Hydrogen Peroxide Tank Pressurization

Challenges and Issues of Modern Science
Purpose. This study develops a pressurization system for hydrogen peroxide tanks using a hybrid gas generator powered by liquid oxygen and solid fuel.
Mykhailo Vorobei, Mykola Bondarenko
doaj