Author: Ulysse J. Blanchard
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
Landing Characteristics of a Lentiucular-shaped Reentry Vehicle
Landing Characteristics of a Lenticular-shaped Re-entry Vehicle
Author: Ulysse J. Blanchard
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
Book Description
Hard-surface landing characteristics of a lenticular-shaped re-entry vehicle obtained with the curved lower surface (heat shield) used as a skid- rocker were good and resulted in maximum normal and angular accelerations of 5g and 18 radians per second squared, respectively, over a range of landing conditions. Horizontal landings in water resulted in large and violent rebounds or dives, depending on the sea conditions or the point of the wave contacted. The nature of the rebounds was such that the attitude of subsequent impacts was random. The maximum longitudinal accelerations obtained in water landings were 10g, maximum normal accelerations were 21g, and maximum angular accelerations were 145 radians per second squared, in waves 7 ft. high (sea state 4). Various auxiliary water-landing devices tested produced no practical improvement in behavior. Reduction of horizontal speed and positive control of impact attitude did improve performance in calm water. During vertical landings (90 degrees flight path) in calm water maximum longitudinal accelerations were 9g, maxim m normal accelerations were 15g, and maximum angular accelerations were 110 radians per second squared for a contact attitude of -45 degrees and a vertical velocity of 70 ft. per sec. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 41
Book Description
Hard-surface landing characteristics of a lenticular-shaped re-entry vehicle obtained with the curved lower surface (heat shield) used as a skid- rocker were good and resulted in maximum normal and angular accelerations of 5g and 18 radians per second squared, respectively, over a range of landing conditions. Horizontal landings in water resulted in large and violent rebounds or dives, depending on the sea conditions or the point of the wave contacted. The nature of the rebounds was such that the attitude of subsequent impacts was random. The maximum longitudinal accelerations obtained in water landings were 10g, maximum normal accelerations were 21g, and maximum angular accelerations were 145 radians per second squared, in waves 7 ft. high (sea state 4). Various auxiliary water-landing devices tested produced no practical improvement in behavior. Reduction of horizontal speed and positive control of impact attitude did improve performance in calm water. During vertical landings (90 degrees flight path) in calm water maximum longitudinal accelerations were 9g, maxim m normal accelerations were 15g, and maximum angular accelerations were 110 radians per second squared for a contact attitude of -45 degrees and a vertical velocity of 70 ft. per sec. (Author).
Landing Characteristics of a Lentiucular-shaped Reentry Vehicle
Landing Characteristics of a Winged Reentry Vehicle with All-skid Landing Gear Having Yielding-metal Shock Absorbers
Author: Ulysee J. Blanchard
Publisher:
ISBN:
Category : Landing gear
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Landing gear
Languages : en
Pages : 52
Book Description
NASA Technical Note
Investigation of the Landing Characteristics of a Reentry Vehicle Having a Canted Multiple-air-bag Load-alleviation System
Author: Sandy M. Stubbs
Publisher:
ISBN:
Category : Impact
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Impact
Languages : en
Pages : 32
Book Description
Water Landing Characteristics of a Model of a Winged Reentry Vehicle
Author: Sandy M. Stubbs
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Static Longitudinal Stability and Control Characteristics at a Mach Number of 1.99 of a Lenticular-shaped Reentry Vehicle
Investigation of the Landing Characteristics of a Reentry Vehicle Having a Canted Multiple-air-bag Load-alleviation System
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description