Little Joe 1A
Little Joe 1A (LJ-1A) was an unmanned rocket launched as part of NASA's Mercury program on November 4, 1959. This flight, a repeat of the Little Joe 1 (LJ-1) launch, was to test a launch abort under high aerodynamic load conditions. After lift-off, the pressure sensing system was to indicate when the correct abort dynamic pressure was reached. This should have happened about thirty seconds after launch. A signal was sent to the explosive bolts to separate the spacecraft from the launch vehicle. Up to this point, everything was going as planned. The impulse was also intended to ignite the escape motor. The motor was ignited, but it took a number of seconds to build up thrust, and thus the abort maneuver was not accomplished at the desired dynamic pressure. Because of this, a repeat of the t
next mission
previous mission
Link from a Wikipage to another Wikipage
next mission
previous mission
primaryTopic
Little Joe 1A
Little Joe 1A (LJ-1A) was an unmanned rocket launched as part of NASA's Mercury program on November 4, 1959. This flight, a repeat of the Little Joe 1 (LJ-1) launch, was to test a launch abort under high aerodynamic load conditions. After lift-off, the pressure sensing system was to indicate when the correct abort dynamic pressure was reached. This should have happened about thirty seconds after launch. A signal was sent to the explosive bolts to separate the spacecraft from the launch vehicle. Up to this point, everything was going as planned. The impulse was also intended to ignite the escape motor. The motor was ignited, but it took a number of seconds to build up thrust, and thus the abort maneuver was not accomplished at the desired dynamic pressure. Because of this, a repeat of the t
mission duration (μ)
0.00568287037037037
has abstract
Little Joe 1A (LJ-1A) foi terc ...... com uma carga útil de 1007 kg.
@pt
Little Joe 1A (LJ-1A) war ein ...... Die Nutzlast betrog 1.007 kg.
@de
Little Joe 1A (LJ-1A) was an u ...... 11 seconds. Payload 1,007 kg.
@en
Little Joe 1A (LJ-1A) è una mi ...... ortata in volo fu di 1.007 kg.
@it
Little Joe 1A byl testovací le ...... ux a 4x pomocný motor Recruit.
@cs
Литл Джо-1A (LJ-1A) — Габаритн ...... АСА, NSSDC ID - Little Joe 1A.
@ru
リトル・ジョー1A号(リトル・ジョー1Aごう、英: Litt ...... 4キロメートルに達し、搭載重量は1,007キログラムだった。
@ja
landing date
1959-11-04
launch date
1959-11-04
launch vehicle
manufacturer
mission duration (s)
next mission
operator
previous mission
Wikipage page ID
page length (characters) of wiki page
Wikipage revision ID
1,014,823,779
Link from a Wikipage to another Wikipage
insignia
@en
landing date
launch date
launch rocket
manufacturer
mission duration
mission type
Abort test
@en
name
Little Joe 1A
@en
next mission
operator
previous mission
programme
(Abort Tests)
@en
spacecraft type
Mercury boilerplate
@en
wikiPageUsesTemplate
hypernym
comment
Little Joe 1A (LJ-1A) foi terc ...... tudo se passou como planejado.
@pt
Little Joe 1A (LJ-1A) war ein ...... 1B ein Affe befördert werden.
@de
Little Joe 1A (LJ-1A) was an u ...... use of this, a repeat of the t
@en
Little Joe 1A (LJ-1A) è una mi ...... o dagli Stati Uniti d'America.
@it
Little Joe 1A byl testovací le ...... km a dosáhla rychlosti 3254 k
@cs
Литл Джо-1A (LJ-1A) — Габаритн ...... АСА, NSSDC ID - Little Joe 1A.
@ru
リトル・ジョー1A号(リトル・ジョー1Aごう、英: Litt ...... 4キロメートルに達し、搭載重量は1,007キログラムだった。
@ja
label
Little Joe 1A
@cs
Little Joe 1A
@en
Little Joe 1A
@it
Little Joe 1A
@pt
Mercury-Little Joe 1A
@pl
Mercury-Little-Joe 1A
@de
Литл Джо-1A
@ru
リトル・ジョー1A号
@ja
sameAs
wasDerivedFrom
isPrimaryTopicOf
name
Little Joe 1A
@en