I am having a devil of a time finding detailed information on the Voyager 1 and 2 launches.
Voyager 1 was lunched September 5, 1977. This web page from the National Space Science Data Center gives some good details on Voyager's interplentary trajectory.
http://nssdc.gsfc.nasa.gov/nmc/spacecraftOrbit.do?id=1977-084A
This NSSDC page starts the inital leg of the interplentary cruise ("Central Body: Sun") on September 8, about 68 hours after launch.
The NASA/JPL web page for Voyager gives the same date, calling it "Earth Injection to Jupiter"
http://voyager.jpl.nasa.gov/science/hyperbolic.html
There is a similar 3 day lag (closer to 69 hours) between launch and interplanetary flight for Voyager 2.
My initial though was that the Voyagers spent 3 days in a parking orbit, but I had my doubts. I got looking into the Centaur D-1T booster. It was fueled with liquid oxygen and hydorgen, and these cryogenic fuels tend to boil off pretty quickly. I found reports of early test flights for the D-1T, from the mid-70s, and NASA was thrilled to get 7 1/2 hours coast time between engine firings.
So what is that 3-day lag between launch and "interplanetary flight" (or "Earth injection to Jupiter" depending on the source terminalogy)? Could the Voyagers have taken that much time to leave Earth's shpere of influence? That seems like an awfully slow flight. Or, by 1977, could the Centaur's coast time have been extended, with the injection burn taking place 3 days after launch? That seems like an awfully long parking orbit coast. (Although Clementine in 1998 coasted for a week in Earth orbit before beginning its boost to the Moon, so a long parking orbit coast is not unheard of.)
I do have solid information that the Viking missions, launched with the same model Titan/Centaur rocket in 1975, had maximum coast times of 28 minutes. So I am leaning toward the short coast and long time to leave Earth's SOI.
It is frustrating to have such sketchy information on the launch trajectories details for such a significant mission -- hardest Orbiter historical detective work I have ever done.
Any thoughts?
Voyager 1 was lunched September 5, 1977. This web page from the National Space Science Data Center gives some good details on Voyager's interplentary trajectory.
http://nssdc.gsfc.nasa.gov/nmc/spacecraftOrbit.do?id=1977-084A
This NSSDC page starts the inital leg of the interplentary cruise ("Central Body: Sun") on September 8, about 68 hours after launch.
The NASA/JPL web page for Voyager gives the same date, calling it "Earth Injection to Jupiter"
http://voyager.jpl.nasa.gov/science/hyperbolic.html
There is a similar 3 day lag (closer to 69 hours) between launch and interplanetary flight for Voyager 2.
My initial though was that the Voyagers spent 3 days in a parking orbit, but I had my doubts. I got looking into the Centaur D-1T booster. It was fueled with liquid oxygen and hydorgen, and these cryogenic fuels tend to boil off pretty quickly. I found reports of early test flights for the D-1T, from the mid-70s, and NASA was thrilled to get 7 1/2 hours coast time between engine firings.
So what is that 3-day lag between launch and "interplanetary flight" (or "Earth injection to Jupiter" depending on the source terminalogy)? Could the Voyagers have taken that much time to leave Earth's shpere of influence? That seems like an awfully slow flight. Or, by 1977, could the Centaur's coast time have been extended, with the injection burn taking place 3 days after launch? That seems like an awfully long parking orbit coast. (Although Clementine in 1998 coasted for a week in Earth orbit before beginning its boost to the Moon, so a long parking orbit coast is not unheard of.)
I do have solid information that the Viking missions, launched with the same model Titan/Centaur rocket in 1975, had maximum coast times of 28 minutes. So I am leaning toward the short coast and long time to leave Earth's SOI.
It is frustrating to have such sketchy information on the launch trajectories details for such a significant mission -- hardest Orbiter historical detective work I have ever done.
Any thoughts?