INVESTIGATION OF MECHANISM OF POTENTIAL AIRCRAFT FUEL TANK VENT FIRES AND EXPLOSIONS CAUSED BY ATMOSPHERIC ELECTRICITY.
Aircraft fires and explosions caused by atmosphere electricity at fuel tank vents
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Aircraft fires and explosions caused by atmosphere electricity at fuel tank vents
Influence of venting and gas leakage on tracking of orbital vehicles
Bubble mechanics, boiling heat transfer, and propellant tank venting in zero gravity environment - storage and handling of cryogenic liquid propellants in orbit
Vent subsystem design specifications for use in fuel cell assembly
Low gravity liquid hydrogen tank venting, considering systems with heat exchange for space missions
A Solid-State Thermodynamic Vent System (STVS) is a novel Cryogenic Fluid Management (CFM) technology for spacecraft cryogenic propellant tanks that may reduce boiloff while providing greater control over the propellant condition. By exploiting the vacuum-induced cryocooling (VIC) potential of cryogen-saturated silica aerogel material, an internal STVS heat exchanger (HX) can expel some sacrificial cryogenic propellant to the vacuum of space to produce cooling within the storage tank. This cooling is transferred directly to the stored fluid, thereby reducing boiloff and increasing hold times. Testing proved the effectiveness of the concept by reducing the liquid nitrogen (LN 2 ) boiloff rate and tank pressure by roughly 70% and 77%, respectively, during a single pump-down cycle, which sacrificed around 1.8 kg of propellant.
Explore multi-layer blanket insulation venting for blankets 4-6 times larger than procedure guideline specifications.
Precipitation may form in humid containers undergoing rapid depressurization. This precipitation may be liquid, i.e. fog, if the dewpoint is crossed above the freezing point of water, or direct snow crystallization if the dewpoint is crossed below the freezing point. Accurate modeling of this effect is potentially important for rapidly ascending vented containers in aircraft, spacecraft, and launch vehicles, as well as rapidly depressurizing vacuum chambers. A transient thermodynamics model of precipitation formation during the rapid depressurization of a container was developed in python. The model is written for a generic container and includes an optional water pool and water vapor source. Details of the model and results from several example cases spanning the full capabilities of the model, including a validation case, will be presented. Although the model is not novel, in contrast to prior works, this one was treated as a case study of the assistance of AI Large Language Models (LLMs) to create physical models. Impressions, performance, time, and cost of using AI for this task will be discussed.
Mechanisms of potential aircraft fuel tank vent fires and explosions caused by atmospheric electricity
Cryogenic propellant venting under low pressure conditions - heat-transfer coefficients for two- phase, single component, solid-gas mixture flow in short, vertical tube
Saturn V/S-IVB stage low gravity fluid mechanics problems and Saturn IB liquid hydrogen orbital experiment to verify propellant ullaging and orbital venting system
Striated cone structure resembling shatter cones in volcanic vent near Albuquerque, New Mexico
Hydrogen vent flare stack performance in adverse weather conditions
Low leakage rate, large diameter vent and relief valve operates satisfactorily over a large temperature range by a design that accommodates waviness and distortions due to thermal gradients. It is based on a fixed sealing member having an inclined lapped surface to which a flexible flow gate conforms.
Wall temperatures and heat transfer coefficients for solid-vapor mixtures of para hydrogen and nitrogen venting under low pressure
Computer program to determine pressure and pipe flow heat transfer in vented launch vehicle compartments during ascending flight
Characteristics of liquid metal cooled reactor gaseous fission products vented or contained, for space power systems
Supersonic wind tunnel tests of orifice venting characteristics and three dimensional flow on flat plates