Update: We have moved websites! Visit our new blog (www.launchwithus.org) to stay up to date with the latest HAB news and articles, including the latest versions of our tools and estimators.
While your High Altitude Balloon (HAB) payload may not be as critical as an Apollo mission returning from space, it still requires careful thought and planning. It is important that you balance the trade-offs such as a safe impact speed (slower descent) with a longer descent time and travel distance (faster descent is more desirable).
This Space Camp post is intended to give you all the background and tools required to estimate what size parachute is suitable for your HAB mission. To cut straight to the chase, our HAB Parachute Size Estimator tool is provided here. For background on the assumptions that go into these calculations and to learn more details about the math behind the spreadsheet, please read on!
The amateur HAB enthusiast has a lot of questions pulsing through their mind. How big does my parachute need to be? What size balloon do I need, and how high will it go? How do I track my HAB? Stay tuned for the answers to each of these, but we hope to at least address the first question in this post.
HAB Parachute Size Estimator
We created this spreadsheet to assist HAB users in determining what size parachute is required for a successful HAB launch. Key instructions to operating this spreadsheet are provided below, and as always, please submit any and all feedback for improvements and future capabilities to firstname.lastname@example.org!
- Enter your payload weight in Cell C4
- Voila! The spreadsheet will provide an estimate for the range of parachute sizes you should consider.
- Click on the “Chute Calcs” Sheet to trigger advanced options.
- Adjust the landing altitude density in Cell C5, if you are considerably higher than sea level (Note: even from sea level to Denver, CO, it will only change your diameter by roughly 3 inches, so it can be neglected for a rough estimate)
- In addition to the above, adjust your payload cross-sectional drag area (Cell C9) and drag coefficient (cell C10), if the shape is much different than a standard cube
- Iterate based on the recommended parachute size to adjust the Parachute Weight (Cell C13)
- Adjust your target landing impact speeds in Cell C3 and C4, if desired. Note: between ~11-16 mph is recommended as a good balance between shorter landing time and safe impact speed.
Types of Parachutes
The typical parachute you are likely used to seeing have a conical or hemi-spherical shape while inflated. There are many different types of parachutes, with each having its own advantages in certain applications. Below is a short listing of some common (and not so common) types of parachutes, with the major emphasis on the first type (flat circular) for HAB launches.
Flat Circular Parachute – these parachutes are extremely common in HAB and hobby rocketry fields due to their ease of manufacture, simple design, and reliability. The trade-off is that the draft coefficient (Cd) is not as high for a given cloth diameter. For the price and for HAB applications, it is hard to go wrong with a flat circular (or flat hexagonal, as we use) parachute. Typical drag coefficients range from 0.75-0.80.
Other Parachutes – a short list of other parachute designs and typical drag coefficient ranges is presented below from Knacke’s Parachute Recovery Systems Design Manual (1991).
To determine the impact speed of your parachute, we are interested in solving for the descent velocity that results in the Drag force equaling out your payload weight, meaning that all forces are equal and the parachute is not accelerating (constant speed at impact). The governing equation is:
W=payload (+ parachute) weight
rho = atmospheric density
V = velocity
S = drag area (for parachute, Circular Area = Pi*radius^2)
CD = drag coefficient
Thus, our spreadsheet provides known values or estimates for all the above variables, and then calculates the resulting radius (and diameter) of the parachute to result in a desired landing speed.
There are various assumptions that are inherent in this spreadsheet and that were assumed for simplification purposes. Some of them are listed here for your awareness:
- Drag and Weight of the parachute and balloon itself on descent are assumed to cancel out. This varies from flight to flight. Also, if your balloon entangles the parachute lines or happens to generate more (or less) drag than predicted, this can affect your descent predictions. We have found through experience that this typically cancels out, but one way to ensure the balloon does not affect descent would be to include some type of cut-down mechanism to sever the balloon after it bursts.
- Assumes sea-level landing, standard day conditions. If the conditions are extreme (either hot or cold) and the altitude varies significantly from sea level (e.g. at high altitude), this can affect the estimated impact velocity.
- Assumes no vertical component of wind. Wind can affect descent results.
- Assumes that our standard offering of a Top Flight Recovery LLC parachute is used. Different parachutes will offer different drag characteristics that must be accounted for (size, shape, porosity, line length to payload, etc. all affect drag coefficient)