Results 121 to 130 of about 8,057 (291)
EFFECT OF BUOYANCY ON FUEL CONTAINMENT IN AN OPEN-CYCLE GAS-CORE NUCLEAR ROCKET ENGINE [PDF]
, 1971 H. A. Putre
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Similarity Assessment of the Engineering Concepts: Decision‐Making Support and Metrics
Systems Engineering, EarlyView.ABSTRACT The new product development (NPD) process is a systematic approach to bring new products and innovations to market. Nowadays, this process is affected by a number of influencing factors associated with the fast‐paced technological changes. One of those factors is the distributed design nature of product development activities: team members are
Yaroslav Menshenin +3 more
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Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance, [PDF]
, 1979 R. A. Bjorklund +2 more
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Spiral Approach for Non‐Software Product and Engineering System Development
Systems Engineering, EarlyView.ABSTRACT This article explored the spiral development process, sometimes called “evolutionary acquisition” in military sectors, and reviewed major non‐software applications in the engineering literature. The spiral development process was originally developed for the design of software while minimizing and managing risk, but the principles can be ...
Isha Amod Gujarathi +2 more
wiley +1 more source
The performance and application of high speed long life LH2 hybrid bearings for reusable rocket engine turbomachinery [PDF]
, 1983 N. P. Hannum, C. E. Nielson
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IET Smart Energy Systems, EarlyView.This review focuses on the recent advances in the key research and technology development of transcritical CO2 heat pumps and integrated energy systems including sustainable ‘green’ heating, energy storage, electro‐thermal storage, waste heat recovery and disruptive electrification of renewable energy, combined heating and power, and new hybrid systems.
Lixin Cheng, Hongzhi Li, Haijun Wang
wiley +1 more source
Preliminary evaluation of nuclear hazards associated with orbital start of a nuclear rocket engine
, 1964 openalex +2 more sources
Comparison of two procedures for predicting rocket engine nozzle performance [PDF]
, 1987 Ken Davidian
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