QTV (Qualification Test Vehicle) was the first test flight of the

Apollo Apollo, grc, Ἀπόλλωνος, Apóllōnos, label=genitive , ; , grc-dor, Ἀπέλλων, Apéllōn, ; grc, Ἀπείλων, Apeílōn, label= Arcadocypriot Greek, ; grc-aeo, Ἄπλουν, Áploun, la, Apollō, la, Apollinis, label ...

Little Joe II Little Joe II was an American rocket used from 1963 to 1966 for five uncrewed tests of the Apollo spacecraft launch escape system (LES), and to verify the performance of the command module parachute recovery system in abort mode. It was name ...

rocket. It was launched in August 1963.

Objectives

The

Qualification Test Vehicle was launched on its first flight from

White Sands Missile Range White Sands Missile Range (WSMR) is a United States Army military testing area and firing range located in the US state of New Mexico. The range was originally established as the White Sands Proving Ground on 9July 1945. White Sands National P ...

New Mexico ) , population_demonym = New Mexican ( es, Neomexicano, Neomejicano, Nuevo Mexicano) , seat = Santa Fe , LargestCity = Albuquerque , LargestMetro = Tiguex , OfficialLang = None , Languages = English, Spanish ( New Mexican), Navajo, Ke ...

, Area # 3. The mission objectives were to prove the Little Joe II rocket's capability as an

Apollo CSM The Apollo command and service module (CSM) was one of two principal components of the United States Apollo spacecraft, used for the Apollo program, which landed astronauts on the Moon between 1969 and 1972. The CSM functioned as a mother shi ...

test vehicle and to determine base pressures and heating on the

rocket A rocket (from it, rocchetto, , bobbin/spool) is a vehicle that uses jet propulsion to accelerate without using the surrounding air. A rocket engine produces thrust by reaction to exhaust expelled at high speed. Rocket engines work entirely fr ...

Flight

Little Joe II QTV was the first flight of the Little Joe II rockets. It was launched from White Sands Missile Range, New Mexico on August 28, 1963 from Launch Complex 36, Area number 3. The vehicle payload consisted of a simulated

command and service module The Apollo command and service module (CSM) was one of two principal components of the United States Apollo spacecraft, used for the Apollo program, which landed astronauts on the Moon between 1969 and 1972. The CSM functioned as a mother sh ...

(rather than a boilerplate spacecraft, as used on later test flights) and an inert

launch escape system A launch escape system (LES) or launch abort system (LAS) is a crew-safety system connected to a space capsule that can be used to quickly separate the capsule from its launch vehicle in case of an emergency requiring the abort of the launch, suc ...

. Most objectives were achieved. The lone failure was a malfunction in the destruct system.

References

Little Joe II Qualification Test Flight Report - September 1963 (PDF)

External links

Little Joe II Progress Report - December 1964 (PDF)Little Joe II Mission A-003 - April 1965 (PDF)
Apollo program 1963 in spaceflight Test spaceflights {{space-stub