Delta-P
The Delta-P is an American rocket stage, developed by McDonnell Douglas and TRW, first used on November 10, 1972 as the second stage for the Delta 1000 series.It continued to serve as the second stage for subsequent Delta 2000 and Delta 3000 flights for 17 years, with its last usage on February 8, 1988.It is propelled by a single TRW TR-201 rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic.
primaryTopic
Delta-P
The Delta-P is an American rocket stage, developed by McDonnell Douglas and TRW, first used on November 10, 1972 as the second stage for the Delta 1000 series.It continued to serve as the second stage for subsequent Delta 2000 and Delta 3000 flights for 17 years, with its last usage on February 8, 1988.It is propelled by a single TRW TR-201 rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic.
has abstract
Delta-P – górny człon rakiet n ...... 000, Delta 5000 oraz Delta II.
@pl
O Delta P foi uM foguete espac ...... ágio de vários foguetes Delta.
@pt
The Delta-P is an American roc ...... 5000, and subsequent Delta II.
@en
Wikipage page ID
39,956,828
Wikipage revision ID
739,437,997
country-origin
fuel
manufacturer
TRW and McDonnell Douglas
time
subject
hypernym
type
comment
Delta-P – górny człon rakiet n ...... siężycowego z programu Apollo.
@pl
O Delta P foi uM foguete espac ...... ágio de vários foguetes Delta.
@pt
The Delta-P is an American roc ...... troxide, which are hypergolic.
@en
label
Delta P
@pt
Delta-P
@en
Delta-P
@pl