This paper presents a derivation of the opening shock factor (Ck) and inflation duration (tfill) that characterize the inflation of slider-reefed parafoils. The results apply to large-mass ratio systems, such as personnel parachutes, that inflate along a downward vertical trajectory and experience maximum drag (Fmax) during slider-descent. The derivation of Ck is based on a formulas derived from the well-validated inflation computer model discussed in another paper presented at this conference (see paper 2007-2501). The formula for tfill is obtained by merging this result with a general expression for Ck, obtained from the Momentum-Impulse theorem in which the inflation time is a crucial input. These derivations are followed by an altitude-...
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shape...
The pressure variation inside the launch vehicle fairing during climb through the atmosphere induces...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
This paper discusses the definition and validation of an upgraded model of slider-reefed parafoil in...
The opening shock factor Ck is a dimensionless formulation of a parachute’s maximum drag generated d...
We describe a new calculation of the opening shock factor C (sub k) characterizing the inflation per...
The minimum inflation pressure and volume are key characteristics of an IAD design because the mass ...
This paper presents a more accurate approximation of the mathematical relationship between riser ten...
The extra-large parachutes were different from the common parachutes because of their size and openi...
The attainability of the opening process directly determines the success of a ram-air parachute aird...
In this paper, a new empirical indicator for predicting the peak opening loads of supersonic parachu...
Data from the Orion and several other test programs have been used to reconstruct inflation paramete...
The role of apparent mass effects in determining the magnitude of parachute opening shock force have...
A two-body computerized mathematical model is used to calculate planar dynamics of the LADT #3 and s...
AbstractA direct numerical modeling method for parachute is proposed firstly, and a model for the st...
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shape...
The pressure variation inside the launch vehicle fairing during climb through the atmosphere induces...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...
This paper discusses the definition and validation of an upgraded model of slider-reefed parafoil in...
The opening shock factor Ck is a dimensionless formulation of a parachute’s maximum drag generated d...
We describe a new calculation of the opening shock factor C (sub k) characterizing the inflation per...
The minimum inflation pressure and volume are key characteristics of an IAD design because the mass ...
This paper presents a more accurate approximation of the mathematical relationship between riser ten...
The extra-large parachutes were different from the common parachutes because of their size and openi...
The attainability of the opening process directly determines the success of a ram-air parachute aird...
In this paper, a new empirical indicator for predicting the peak opening loads of supersonic parachu...
Data from the Orion and several other test programs have been used to reconstruct inflation paramete...
The role of apparent mass effects in determining the magnitude of parachute opening shock force have...
A two-body computerized mathematical model is used to calculate planar dynamics of the LADT #3 and s...
AbstractA direct numerical modeling method for parachute is proposed firstly, and a model for the st...
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shape...
The pressure variation inside the launch vehicle fairing during climb through the atmosphere induces...
Free-body tests were made in the Langley spin tunnel to determine drag coefficients for 1.07-meter-d...