Estes C5-3 motors available

The Rocketry Forum

Help Support The Rocketry Forum:

This site may earn a commission from merchant affiliate links, including eBay, Amazon, and others.
It was allowed back then. Now that I think about it, I wonder if an A10-0T would be enough to cut the string and release the blades without the delay?
As of this post, Estes still has A10-0T in stock.

An early deploy would seem to be less likely to cause a lawn dart.
 
As of this post, Estes still has A10-0T in stock.

An early deploy would seem to be less likely to cause a lawn dart.
But is the A10-0T ejection enough to burn through the thin string that holds the blades in place? The Estes site only recommends A10-3T.

The main problem is that I need to add a frak ton of weight in the NC for the Heli to fly straight up. This tends to make it keel over at apogee so any delay is bad.
 
But is the A10-0T ejection enough to burn through the thin string that holds the blades in place? The Estes site only recommends A10-3T.

The main problem is that I need to add a frak ton of weight in the NC for the Heli to fly straight up. This tends to make it keel over at apogee so any delay is bad.
I'd look to other solutions for your HD problem. However, the A10-0t can definitely burn through a string to release a recovery system.
 
Unless you "improve" the Mini-A Heli by making it heavier, it works fine on A10-3Ts. If you piston-launch it, it even works well on 1/2A3-2Ts.

Often items "out of stock" will return in a day or two. As has been noted elsewhere, that's out of stock at the corner of one warehouse where the mail-order fulfillment is done, not out of stock in Penrose. That said, I see AC Supply is also out of C5-3s....so maybe they do need to make more.
 
Oh man, I was going to be ordering from AC Supply in the next few weeks and wanted to snag more C5-3s. :(
 
Just ordered C5-3’s and A10-3T’s from Rocketry Works as well

The downside is that Estes is now out of stock on the A-Heli!

Should have ordered the kit last night...

woulda-coulda-shoulda
 
I realized I had more comparisons with the Estes Centuri and Nike Smoke. Both rockets need a longer delay so it can weathercock into the wind and return to the launch site. They definitely flew straighter with the C5-3 and traveled further because of the shorter delay. Overall, I don't think I'll bother using the C5-3 with these rockets and stick with the C6-5.

Timeline:
00:03 Centuri with C6-3
00:43 Centuri with C5-3
01:29 Nike Smoke with C6-5
02:20 Nike Smoke with C5-3

 
Last edited:
Just ordered C5-3’s and A10-3T’s from Rocketry Works as well

The downside is that Estes is now out of stock on the A-Heli!

Should have ordered the kit last night...

woulda-coulda-shoulda
So I found the Mini A Heli kit on sale at HobbyLinc and put in my order for two of them.

Cost me a buck and a half more than Estes in total.
 
Got this e-mail from Estes, as many of you are probably receiving now:

New Product Super C


Not yet available from AC Supply. I think I still have a few "Super C" motors when they were produced by Centuri.
I bought some from Estes recently. Have not flown with them yet.
 
Do they work good for heavier rockets?
Oh yeah!

Per Estes site
For C6 motors, max recommended lift off weight is 113 grams
For C5, 227 grams.

Interestingly, Quest D16 maximum recommended liftoff weight is 128 grams, which seems low to me.

Here is my source, the Quest site

https://www.questaerospace.com/2-Pack_D16-4_Q-Jet_Model_Rocket_Motor/p4193205_18980165.aspx

Here is the RocketReviews side by side comparison

https://www.rocketreviews.com/compare-motors---estes-c5-to-quest-d16-q-jet.html
https://www.rocketreviews.com/compare-motors---estes-c6-to-quest-d16-q-jet.html
 
https://www.rocketreviews.com/compare-estes-c6-to-estes-c5.html
Something I don’t get on the data here, maybe @jadebox or another of many forum members smarter than me can explain.

How come the C6 is rated as 76%C and C5 only 56%C?

How can the C5 have equal propellant (actually slightly more) and lower total impulse?
To me, the area under the curve for the C5 appears to be AT LEAST as much as the C6, and it eyeballs slightly more.

Why is the C5 lighter (larger nozzle bore means less clay,bigger hole?)
 
They are designed to get heavier rockets off the pad faster, improving their stability and reducing weathercocking.
Makes sense..Thank you for the info on the C5. Did the C5 replace the old Estes B14 motor from years ago?
 

Attachments

  • b14.jpg
    b14.jpg
    10.2 KB · Views: 26
Oh yeah!

Per Estes site
For C6 motors, max recommended lift off weight is 113 grams
For C5, 227 grams.

Interestingly, Quest D16 maximum recommended liftoff weight is 128 grams, which seems low to me.

Here is my source, the Quest site

https://www.questaerospace.com/2-Pack_D16-4_Q-Jet_Model_Rocket_Motor/p4193205_18980165.aspx

Here is the RocketReviews side by side comparison

https://www.rocketreviews.com/compare-motors---estes-c5-to-quest-d16-q-jet.html
https://www.rocketreviews.com/compare-motors---estes-c6-to-quest-d16-q-jet.html
I agree what you said on the D16. For a D motor it should be more thrust. Thank you for taking the time for the Motor comparison charts.
 
Interestingly, Quest D16 maximum recommended liftoff weight is 128 grams, which seems low to me.

Here is my source, the Quest site

https://www.questaerospace.com/2-Pack_D16-4_Q-Jet_Model_Rocket_Motor/p4193205_18980165.aspx

Here is the RocketReviews side by side comparison

https://www.rocketreviews.com/compare-motors---estes-c5-to-quest-d16-q-jet.html
https://www.rocketreviews.com/compare-motors---estes-c6-to-quest-d16-q-jet.html
The reason is the delay. Quest D16's are only 12 N-s and the delay is longer so a heavier rocket will need a shorter delay than 4 seconds. Also, Estes seconds are shorter than Aerotech seconds. (Where is the duck smiley?)
 
How can the C5 have equal propellant (actually slightly more) and lower total impulse?
To me, the area under the curve for the C5 appears to be AT LEAST as much as the C6, and it eyeballs slightly more.
The C5 has a deeper core for more initial thrust. This also results in a larger nozzle throat. Due to the larger nozzle, the rest of the propellant burns at a lower pressure and loses some specific impulse. That's why the total impulse is lower even with the same amount of propellant. It also results in a longer, lower thrust burn.
 
The C5 has a deeper core for more initial thrust. This also results in a larger nozzle throat. Due to the larger nozzle, the rest of the propellant burns at a lower pressure and loses some specific impulse. That's why the total impulse is lower even with the same amount of propellant. It also results in a longer, lower thrust burn.
If I understand you correctly, you are saying that the C5 nozzle is less efficient (not knocking you or arguing, I think that makes sense but I was a biology major not an engineering major, so I don’t have the savvy to figure it out myself.). I also understand (I think) that in some cases “less efficient” doesn’t mean “not as good”, in this case it may be less efficient in total impulse but still better for certain applications (like getting big draggy rockets off the pad.). Still, when I look at the the thrust curves, the C5 spike is significantly higher AND slightly longer lasting, and whatever you call the flat part of the curve (“plateau”?) is minimally lower in thrust and the C5 burn is slightly longer. So I am still at a loss, I thought the total impulse was basically the area under the curve. Eyeballing it the C5 looks higher. Also, C5 at 7.79 Ns and C6 at 8.82 gives a ratio of 0.88, while for “Motor Class” C5 at 56% C vs C6 at 76% C gives a ratio of 0.73. So my ignorance is showing again......
 
Last edited:

Latest posts

Back
Top